{
  "Spase": {
    "xmlns:xsi": "http://www.w3.org/2001/XMLSchema-instance",
    "xmlns": "http://www.spase-group.org/data/schema",
    "xsi:schemaLocation": "http://www.spase-group.org/data/schema http://www.spase-group.org/data/schema/spase-2_3_0.xsd",
    "Version": "2.3.2",
    "NumericalData": {
      "ResourceID": "spase://NASA/NumericalData/FAST/MAG/Fluxgate/PT7.8125MS",
      "ResourceHeader": {
        "ResourceName": "FAST Fluxgate Magnetometer High-Resolution 7.8125 ms Data",
        "ReleaseDate": "2021-04-27T15:38:11Z",
        "Description": "Calibrated Fluxgate Data acquired by the Fast Auroral SnapshoT Small Explorer, FAST, Magnetometer Instrument. Data have been calibrated, despun, and detrended against the International Geomagnetic Reference Field, IGRF, using IGRF Coefficients for the Date of Acquisition. Data are provided in several Coordinate Systems. Non detrended Data in Spacecraft and Geocentric Equatorial Inertial Coordinates are provided. Ephemeris Data are also provided.",
        "Acknowledgement": "C.W. Carlson, R.J. Strangeway Include Acknowledgement in any publication.",
        "Contact": [
          {
            "PersonID": "spase://SMWG/Person/Robert.J.Strangeway",
            "Role": "PrincipalInvestigator"
          },
          {
            "PersonID": "spase://SMWG/Person/Robert.E.McGuire",
            "Role": "MetadataContact"
          },
          {
            "PersonID": "spase://SMWG/Person/Lee.Frost.Bargatze",
            "Role": "MetadataContact"
          }
        ],
        "InformationURL": [
          {
            "Name": "FAST Fluxgate Magnetometer High Resolution Data Set Description",
            "URL": "https://cdaweb.gsfc.nasa.gov/FAST_HR_DCB_Document.pdf",
            "Description": "FAST Magnetometer Data Set Description"
          },
          {
            "Name": "FAST Fluxgate Magnetometer Instrument Description Space Science Review Paper",
            "URL": "https://link.springer.com/article/10.1023%2FA%3A1013153623344",
            "Description": "FAST Magnetometer Instrument Description"
          }
        ],
        "PriorID": [
          "spase://VSPO/NumericalData/FAST/DCF/MAG/HR_DCB/PT0.125S",
          "spase://VSPO/NumericalData/FAST/MAG/Fluxgate/PT7.8125MS"
        ]
      },
      "AccessInformation": [
        {
          "RepositoryID": "spase://SMWG/Repository/NASA/GSFC/SPDF",
          "Availability": "Online",
          "AccessRights": "Open",
          "AccessURL": [
            {
              "Name": "FTPS from SPDF (not with most browsers)",
              "URL": "ftps://spdf.gsfc.nasa.gov/pub/data/fast/dcf/l2/dcb/",
              "Description": "Access to Data in CDF Format via ftp from SPDF"
            },
            {
              "Name": "HTTPS from SPDF",
              "URL": "https://spdf.gsfc.nasa.gov/pub/data/fast/dcf/l2/dcb/",
              "Description": "Access to Data in CDF Format via http from SPDF"
            },
            {
              "Name": "CDAWeb",
              "URL": "https://cdaweb.gsfc.nasa.gov/cgi-bin/eval2.cgi?dataset=FAST_HR_DCB&index=sp_phys",
              "ProductKey": "FAST_HR_DCB",
              "Description": "Access to ASCII, CDF, and Plots via NASA/GSFC CDAWeb"
            }
          ],
          "Format": "CDF",
          "Encoding": "None",
          "Acknowledgement": "C.W. Carlson, R.J. Strangeway Include Acknowledgement in any publication. Please acknowledge the Data Providers and CDAWeb when using these Data."
        },
        {
          "RepositoryID": "spase://SMWG/Repository/NASA/GSFC/SPDF",
          "Availability": "Online",
          "AccessRights": "Open",
          "AccessURL": {
            "Name": "CDAWeb HAPI Server",
            "URL": "https://cdaweb.gsfc.nasa.gov/hapi",
            "Style": "HAPI",
            "ProductKey": [
              "FAST_HR_DCB@0",
              "FAST_HR_DCB@1",
              "FAST_HR_DCB@2",
              "FAST_HR_DCB@3"
            ],
            "Description": "Web Service to this product using the HAPI interface."
          },
          "Format": "CSV",
          "Acknowledgement": "C.W. Carlson, R.J. Strangeway Include Acknowledgement in any publication. Please acknowledge the Data Providers and CDAWeb when using these Data."
        }
      ],
      "ProcessingLevel": "Calibrated",
      "InstrumentID": [
        "spase://SMWG/Instrument/FAST/Ephemeris",
        "spase://SMWG/Instrument/FAST/MAG"
      ],
      "MeasurementType": [
        "Ephemeris",
        "InstrumentStatus",
        "MagneticField"
      ],
      "TemporalDescription": {
        "TimeSpan": {
          "StartDate": "1996-09-28T00:45:21.000",
          "StopDate": "1998-10-09T06:21:19.000"
        },
        "Cadence": "PT0.0078125S"
      },
      "Caveats": "Continuous coverage not guaranteed. Check the inventory graph for coverage.",
      "Parameter": [
        {
          "Name": "Epoch Time",
          "ParameterKey": "Epoch",
          "Description": "Epoch Time, Default Time for Processed Data",
          "Caveats": "Time is specified as a Terrestrial Time 2000, TT2000, Variable. Conversion to TT2000 assumes that the Coordinated Universal Time, UTC, as given by the FAST Data Decommutator is correct. This Parameter exhibits an increasing Monotonic Progression.",
          "Cadence": "PT0.0078125S",
          "Units": "ns",
          "UnitsConversion": "1.0e-9>s",
          "RenderingHints": {
            "AxisLabel": "Epoch",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "1990-01-01T00:00:00.000000000",
          "ValidMax": "2030-01-01T00:00:00.999999999",
          "FillValue": "9999-12-31T23:59:59.999999999",
          "Support": {
            "SupportQuantity": "Temporal"
          }
        },
        {
          "Name": "Range Epoch",
          "ParameterKey": "range_epoch",
          "Description": "Range Epoch, CDF Start Time and Stop Time",
          "Caveats": "Start Time and Stop Time for the current CDF File This Parameter exhibits an increasing Monotonic Progression.",
          "Cadence": "PT135M",
          "Units": "ns",
          "UnitsConversion": "1.0e-9>s",
          "RenderingHints": {
            "AxisLabel": "range_epoch",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "1990-01-01T00:00:00.000000000",
          "ValidMax": "2030-01-01T00:00:00.999999999",
          "FillValue": "9999-12-31T23:59:59.999999999",
          "Support": {
            "SupportQuantity": "Temporal"
          }
        },
        {
          "Name": "Delta Magnetic Field Vector, Despun Spacecraft Coordinates, Cartesian",
          "Set": "Time Series defined by using: EPOCH",
          "ParameterKey": "DeltaB_DSC",
          "Description": "Delta Magnetic Field Vector, Despun Spacecraft Coordinates, DSC, Cartesian",
          "Caveats": "Delta Magnetic Field Vector in Despun Spacecraft Coordinates. The Model Magnetic Field Values are calculated by using the International Geomagnetic Reference Field, IGRF, Model Version 11. Despun Spacecraft Coordinates, DSC, are defined as: Z-axis along the Spin Axis, Y-axis in the Spin Plane perpendicular to the Sun Direction, X-axis completing the Triad X-Y-Z. Detrended DeltaB Data have bad Data deleted, DEL_MAG_FLAG equal to 1.",
          "Cadence": "PT0.0078125S",
          "Units": "nT",
          "UnitsConversion": "1.0e-9>T",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "SC"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "DeltaB_DSC",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "dB_dsc_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "dB_dsc_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "dB_dsc_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-100000.0",
          "ValidMax": "100000.0",
          "FillValue": "-1.0e+31",
          "Field": {
            "Qualifier": "Vector",
            "FieldQuantity": "Magnetic"
          }
        },
        {
          "Name": "Delta Magnetic Field Vector, Geocentric Equatorial Inertial Cartesian Coordinates",
          "Set": "Time Series defined by using: EPOCH",
          "ParameterKey": "DeltaB_GEI",
          "Description": "Delta Magnetic Field Vector, Geocentric Equatorial Inertial, GEI, Cartesian Coordinates",
          "Caveats": "DeltaB in Geocentric Equatorial Inertial Coordinates. The Model Magnetic Field Values are calculated by using the International Geomagnetic Reference Field, IGRF, Model Version 11. Detrended DeltaB Data have bad Data deleted, DEL_MAG_FLAG equal to 1.",
          "Cadence": "PT0.0078125S",
          "Units": "nT",
          "UnitsConversion": "1.0e-9>T",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "GEI"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "DeltaB_GEI",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "dB_gei_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "dB_gei_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "dB_gei_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-100000.0",
          "ValidMax": "100000.0",
          "FillValue": "-1.0e+31",
          "Field": {
            "Qualifier": "Vector",
            "FieldQuantity": "Magnetic"
          }
        },
        {
          "Name": "Delta Magnetic Field Vector, Solar Magnetic Cartesian Coordinates",
          "Set": "Time Series defined by using: EPOCH",
          "ParameterKey": "DeltaB_SM",
          "Description": "Delta Magnetic Field Vector, Solar Magnetic, SM, Cartesian Coordinates",
          "Caveats": "DeltaB in Solar Magnetic Coordinates. The Model Magnetic Field Values and the Dipole Axis Direction are calculated by using the International Geomagnetic Reference Field, IGRF, Model Version 11. Detrended DeltaB Data have bad Data deleted, DEL_MAG_FLAG equal to 1.",
          "Cadence": "PT0.0078125S",
          "Units": "nT",
          "UnitsConversion": "1.0e-9>T",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "SM"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "DeltaB_SM",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "dB_sm_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "dB_sm_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "dB_sm_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-100000.0",
          "ValidMax": "100000.0",
          "FillValue": "-1.0e+31",
          "Field": {
            "Qualifier": "Vector",
            "FieldQuantity": "Magnetic"
          }
        },
        {
          "Name": "Delta Magnetic Field Vector, Field-aligned Coordinates, Cartesian",
          "Set": "Time Series defined by using: EPOCH",
          "ParameterKey": "DeltaB_FAC",
          "Description": "Delta Magnetic Field Vector, Field-aligned Coordinates, FAC, o-e-b Cartesian Triad",
          "Caveats": "DeltaB in Field-aligned Coordinates. The Model Magnetic Field is IGRF Version 11. Field-aligned Coordinates, FAC, defined as: 'b' along the Model Magnetic Field, 'e' as East, in the Direction of B-cross-R, and 'o' outwards, completing the Triad o-e-b. Near the Poles 'outwards' points towards the respective north or south Pole. Detrended DeltaB Data have bad Data deleted, DEL_MAG_FLAG equal to 1.",
          "Cadence": "PT0.0078125S",
          "Units": "nT",
          "UnitsConversion": "1.0e-9>T",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "MFA"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "DeltaB_FAC",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "dB_fac_o",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "dB_fac_e",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "dB_fac_b",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-100000.0",
          "ValidMax": "100000.0",
          "FillValue": "-1.0e+31",
          "Field": {
            "Qualifier": "Vector",
            "FieldQuantity": "Magnetic"
          }
        },
        {
          "Name": "Delta Magnetic Field Vector, Field-aligned Spacecraft Coordinates, Cartesian",
          "Set": "Time Series defined by using: EPOCH",
          "ParameterKey": "DeltaB_FAC_V",
          "Description": "Delta Magnetic Field Vector, Field-aligned Spacecraft Coordinates, FAC, v-p-b Cartesian Triad",
          "Caveats": "DeltaB in Field-aligned Spacecraft Coordinates. The Model Magnetic Field is IGRF Version 11. Field-aligned Spacecraft Coordinates use the Spacecraft Velocity Vector, hence DeltaB_FAC_V, in specifying the Coordinate system, which is defined as: 'b' along the Model Magnetic Field, 'p' perpendicular, in the Direction of B-cross-vel_Spacecraft, that is, across Track, and 'v' nominally along the Spacecraft Velocity Vector, along Track, completing the Triad v-p-b. Detrended DeltaB Data have bad Data deleted, DEL_MAG_FLAG equal to 1.",
          "Cadence": "PT0.0078125S",
          "Units": "nT",
          "UnitsConversion": "1.0e-9>T",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "MFA"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "DeltaB_FAC_V",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "dB_fac_v_v",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "dB_fac_v_p",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "dB_fac_v_b",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-100000.0",
          "ValidMax": "100000.0",
          "FillValue": "-1.0e+31",
          "Field": {
            "Qualifier": "Vector",
            "FieldQuantity": "Magnetic"
          }
        },
        {
          "Name": "Delta Magnetic Field Vector, Field-aligned Spin Plane Coordinates, Cartesian",
          "Set": "Time Series defined by using: EPOCH",
          "ParameterKey": "DeltaB_FAC_SP",
          "Description": "Delta Magnetic Field Vector, Field-aligned Spin Plane Coordinates, FAC, s-p-b Cartesian Triad",
          "Caveats": "DeltaB in Field-aligned/Spin Plane Coordinates. The Model Magnetic Field is IGRF Version 11. Field-aligned/Spin Plane Coordinates use the Spin Plane, hence DeltaB_FAC_SP, in specifying the Coordinate system, which is defined as: 'b' along the Model Magnetic Field, 's' in the Spin Axis cross Model Magnetic Field Direction, that is, in the Spin Plane and perpendicular to the Model Field, and 'p' perpendicular (B ⨯ (Spin Axis ⨯ B)), nominally along the Spin Axis, completing the Triad s-p-b. The Spin Plane Coordinate 's' is in the same Direction as the despun Electric Field 'E along V' Component. Note that 'E along V' is nominally along the Spacecraft Velocity only in the northern Hemisphere, and is nominally antiparallel to the Spacecraft Velocity Vector in the southern Hemisphere. The 'E along V' Electric Field crossed with the p-component of 'deltaB_FAC_SP' contributes to the Field-aligned Poynting Flux. In this s-p-b Coordinate system, positive Field-aligned Poynting Flux is into the northern Ionosphere, but away from the southern Ionosphere. The other Contribution to the Field-aligned Poynting Flux would be from the p-component of the Electric Field crossed with the s-component of the DeltaB Magnetic Field, but the p-component of the Electric Field is mainly given by the Spin Axis Electric Field Measurement. Because one of the Axial Booms did not deploy on FAST the Spin Axis Electric Field is generally not used. Detrended DeltaB Data have bad Data deleted, DEL_MAG_FLAG equal to 1.",
          "Cadence": "PT0.0078125S",
          "Units": "nT",
          "UnitsConversion": "1.0e-9>T",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "MFA"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "DeltaB_FAC_SP",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "dB_fac_sp_s",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "dB_fac_sp_p",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "dB_fac_sp_b",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-100000.0",
          "ValidMax": "100000.0",
          "FillValue": "-1.0e+31",
          "Field": {
            "Qualifier": "Vector",
            "FieldQuantity": "Magnetic"
          }
        },
        {
          "Name": "Full Magnetic Field Vector, Geocentric Equatorial Inertial Coordinates",
          "Set": "Time Series defined by using: EPOCH",
          "ParameterKey": "B_GEI",
          "Description": "Full Magnetic Field Vector, Geocentric Equatorial Inertial, GEI, Coordinates",
          "Caveats": "Full non-detrended Magnetometer Data in Geocentric Equatorial Inertial Coordinates, with bad Data deleted, indicated by DEL_MAG_FLAG equal to 1",
          "Cadence": "PT0.0078125S",
          "Units": "nT",
          "UnitsConversion": "1.0e-9>T",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "GEI"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "B_GEI",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "B_gei_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "B_gei_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "B_gei_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-1.0e+08",
          "ValidMax": "1.0e+08",
          "FillValue": "-1.0e+31",
          "Field": {
            "Qualifier": "Vector",
            "FieldQuantity": "Magnetic"
          }
        },
        {
          "Name": "Magnetic Field Data Deletion Flag",
          "Set": "Time Series defined by using: EPOCH",
          "ParameterKey": "DEL_MAG_FLAG",
          "Description": "Magnetic Field Data Deletion Flag",
          "Caveats": "Flags Data that have been deleted in the Magnetic Field Vector Data, B_GEI, and detrended Delta Magnetic Field, DeltaB, Data, or should be deleted from the non-detrended B_DSC and B_SSC Data",
          "Cadence": "PT0.0078125S",
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "DEL_MAG_FLAG",
            "ValueFormat": "I8",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "0",
          "ValidMax": "1",
          "FillValue": "-2147483648",
          "Support": {
            "Qualifier": "Scalar",
            "SupportQuantity": "Other"
          }
        },
        {
          "Name": "Torquer Coil Magnetic Field Vector Data",
          "Set": "Time Series defined by using: EPOCH",
          "ParameterKey": "Torquer",
          "Description": "Estimated Torquer Coil Magnetic Field Vector Data",
          "Caveats": "Estimated Torquer Coil Magnetic Field, in spinning Spacecraft Coordinates. Units are pseudo nT since the Field is estimated with intermediate Data.",
          "Cadence": "PT0.0078125S",
          "Units": "nT",
          "UnitsConversion": "1.0e-9>T",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "SC"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "Torquer",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "Torq_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "Torq_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "Torq_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-1.0e+08",
          "ValidMax": "1.0e+08",
          "FillValue": "-1.0e+31",
          "Field": {
            "Qualifier": "Vector",
            "FieldQuantity": "Magnetic"
          }
        },
        {
          "Name": "Time varying Tweaker Matrix",
          "Set": "Time Series defined by using: EPOCH",
          "ParameterKey": "Tweaker",
          "Description": "Time varying Tweaker Orthogonalization Matrix",
          "Caveats": "Time varying Tweaker Matrix that gives final Orthogonalization and removes Spin Plane Offsets. Tweaker takes into account on Orbit Variations caused by Eclipse Entry, etc. TW_ZX is used to remove from the Z-sensor any Spin Tone Signals in Phase with the X-sensor. TW_ZY is used to remove from the Z-sensor any Spin Tone Signals in Phase with the Y-sensor. TW_YY is used to make the Y-sensor have the same Gain as the X-sensor. TW_YX is used to remove from the Y-sensor any Spin Tone Signals in Phase with the X-sensor. O_X is used to remove any DC Offsets from the X-sensor. O_Y is used to remove any DC Offsets from the Y-sensor.",
          "Cadence": "PT0.0078125S",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "SC"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "Tweaker",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "6",
            "Element": [
              {
                "Name": "TW_ZX",
                "Index": "1",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "TW_ZY",
                "Index": "2",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "TW_YY",
                "Index": "3",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              },
              {
                "Name": "TW_YX",
                "Index": "4",
                "RenderingHints": {
                  "AxisLabel": "4"
                }
              },
              {
                "Name": "O_X",
                "Index": "5",
                "RenderingHints": {
                  "AxisLabel": "5"
                }
              },
              {
                "Name": "O_Y",
                "Index": "6",
                "RenderingHints": {
                  "AxisLabel": "6"
                }
              }
            ]
          },
          "ValidMin": "-1000.0",
          "ValidMax": "1000.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": "Tensor",
            "SupportQuantity": "Other"
          }
        },
        {
          "Name": "Magnetometer Data Quality Flag",
          "Set": "Time Series defined by using: EPOCH",
          "ParameterKey": "MAG_QUAL_FLAG",
          "Description": "Magnetometer Data Quality Flag",
          "Caveats": "The Magnetometer Data Quality Flags are additive. Flag Values 1 to 16 are Torquer and other Data Processing Flags. Flag Values 32 to 2048 are Flags related to Spin Phase Issues. Any Data with a Flag Value 2048 or greater should be used with care. Flag Values: 0=Good, 1=Torquers On, 2=Torquer Ramp, 4=Nutation, to be determined, 8=Reserved, 16=Reserved, 32=Spin Phase Object set to Zero, 64=In Eclipse, using Nadir Table, 128=Reserved, 256=Reserved, 512=Spin Phase Data not smoothed, 1024=Spin Phase Data patched with Nadir or Mission Unique Electronics, MUE, Phase Data, 2048=Missing Spin Phase Data.",
          "Cadence": "PT0.0078125S",
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "MAG_QUAL_FLAG",
            "ValueFormat": "I8",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "0",
          "ValidMax": "4096",
          "FillValue": "-2147483648",
          "Support": {
            "Qualifier": "Scalar",
            "SupportQuantity": "Other"
          }
        },
        {
          "Name": "Full Magnetic Field Vector, Despun Spacecraft Coordinates",
          "Set": "Time Series defined by using: EPOCH",
          "ParameterKey": "B_DSC",
          "Description": "Full Magnetic Field Vector, Despun Spacecraft Coordinates, DSC",
          "Caveats": "Full non-detrended Magnetometer Data in Despun Spacecraft Coordinates (DSC), with bad Data included, indicated by DEL_MAG_FLAG equal to 1. Despun Spacecraft Coordinates have the Z-axis along the nominal Spin Axis, and the Sun in the X-Z Plane.",
          "Cadence": "PT0.0078125S",
          "Units": "nT",
          "UnitsConversion": "1.0e-9>T",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "SC"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "B_DSC",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "B_dsc_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "B_dsc_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "B_dsc_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-1.0e+08",
          "ValidMax": "1.0e+08",
          "FillValue": "-1.0e+31",
          "Field": {
            "Qualifier": "Vector",
            "FieldQuantity": "Magnetic"
          }
        },
        {
          "Name": "Full Magnetic Field Vector, spinning Spacecraft Coordinates",
          "Set": "Time Series defined by using: EPOCH",
          "ParameterKey": "B_SSC",
          "Description": "Full Magnetic Field Vector, spinning Spacecraft Coordinates, SSC",
          "Caveats": "Full non-detrended Magnetometer Data in spinning Spacecraft Coordinates, SSC, with bad Data included, indicated by DEL_MAG_FLAG equal to 1",
          "Cadence": "PT0.0078125S",
          "Units": "nT",
          "UnitsConversion": "1.0e-9>T",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "SR"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "B_SSC",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "B_ssc_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "B_ssc_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "B_ssc_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-1.0e+08",
          "ValidMax": "1.0e+08",
          "FillValue": "-1.0e+31",
          "Field": {
            "Qualifier": "Vector",
            "FieldQuantity": "Magnetic"
          }
        },
        {
          "Name": "Removed Magnetic Field Vector, Spin Tone Harmonic, Despun Spacecraft Coordinates",
          "Set": "Time Series defined by using: EPOCH",
          "ParameterKey": "Bharmonic_DSC",
          "Description": "Removed Magnetic Field Vector, Spin Tone Harmonic, Despun Spacecraft Coordinates, DSC",
          "Caveats": "Magnetic Field Spin Tone Harmonic in Despun Spacecraft Coordinates (DSC). Bad Data removed, DEL_MAG_FLAG equal to 1.",
          "Cadence": "PT0.0078125S",
          "Units": "nT",
          "UnitsConversion": "1.0e-9>T",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "SC"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "Bharmonic_DSC",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "Bharmonic_dsc_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "Bharmonic_dsc_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "Bharmonic_dsc_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-1.0e+08",
          "ValidMax": "1.0e+08",
          "FillValue": "-1.0e+31",
          "Field": {
            "Qualifier": "Vector",
            "FieldQuantity": "Magnetic"
          }
        },
        {
          "Name": "Default Time, Spin Data",
          "ParameterKey": "Spin_Epoch",
          "Description": "Default Epoch Time, Spin Phase and Spin Frequency Data",
          "Caveats": "Time is specified as a TT2000 Variable. Conversion to TT2000 assumes the UTC as given by the FAST Data Decommutator is correct. This Parameter exhibits an increasing Monotonic Progression.",
          "Cadence": "PT15S",
          "Units": "ns",
          "UnitsConversion": "1.0e-9>s",
          "RenderingHints": {
            "AxisLabel": "Spin_Epoch",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "1990-01-01T00:00:00.000000000",
          "ValidMax": "2030-01-01T00:00:00.999999999",
          "FillValue": "9999-12-31T23:59:59.999999999",
          "Support": {
            "SupportQuantity": "Temporal"
          }
        },
        {
          "Name": "Spin Frequency",
          "Set": "Time Series defined by using: SPIN_EPOCH",
          "ParameterKey": "Spin_Freq",
          "Description": "Spacecraft Spin Frequency",
          "Caveats": "Spacecraft Spin Frequency at the Time specified by Spin_Epoch",
          "Cadence": "PT15S",
          "Units": "°/s",
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "Spin_Freq",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "-1000.0",
          "ValidMax": "1000.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": "Scalar",
            "SupportQuantity": "Other"
          }
        },
        {
          "Name": "Spin Phase Angle",
          "Set": "Time Series defined by using: SPIN_EPOCH",
          "ParameterKey": "Spin_Phase",
          "Description": "Spacecraft Spin Phase Angle, Magnetometer X-axis",
          "Caveats": "Phase Angle of the Magnetometer X-axis with respect to the Sun at the Time specified by Spin_Epoch",
          "Cadence": "PT15S",
          "Units": "°",
          "UnitsConversion": "0.0174532925>rad",
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "Spin_Phase",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "-1080.0",
          "ValidMax": "1080.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": "Scalar",
            "SupportQuantity": "Other"
          }
        },
        {
          "Name": "Default Time, Ephemeris Data",
          "ParameterKey": "Ephemeris_Epoch",
          "Description": "Default Epoch Time, Ephemeris Data",
          "Caveats": "Time is specified as a TT2000 Variable. Conversion to TT2000 assumes the UTC as given by the FAST Data Decommutator is correct. Ephemeris Data are usually provided with a 1 s Cadence. This Parameter exhibits an increasing Monotonic Progression.",
          "Cadence": "PT1S",
          "Units": "ns",
          "UnitsConversion": "1.0e-9>s",
          "RenderingHints": {
            "AxisLabel": "Ephemeris_Epoch",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "1990-01-01T00:00:00.000000000",
          "ValidMax": "2030-01-01T00:00:00.999999999",
          "FillValue": "9999-12-31T23:59:59.999999999",
          "Support": {
            "Qualifier": "Scalar",
            "SupportQuantity": "Temporal"
          }
        },
        {
          "Name": "FAST Orbit Number",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "Orbit",
          "Description": "FAST Spacecraft Orbit Number",
          "Caveats": "Orbit Number as specified by the FAST Ephemeris Software, together with the other Ephemeris Information",
          "Cadence": "PT1S",
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "Orbit",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "0.0",
          "ValidMax": "99999.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": "Scalar",
            "SupportQuantity": "Other"
          }
        },
        {
          "Name": "Spacecraft Position, Geocentric Equatorial Inertial Coordinates",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "pos_gei",
          "Description": "Spacecraft Position, Geocentric Equatorial Inertial, GEI, Coordinates",
          "Caveats": "FAST Spacecraft Position in Geocentric Equatorial Inertial Coordinates",
          "Cadence": "PT1S",
          "Units": "km",
          "UnitsConversion": "1.0e3>m",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "GEI"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "pos_gei",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "pos_gei_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "km",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "pos_gei_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "km",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "pos_gei_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "km",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-1.0e+08",
          "ValidMax": "1.0e+08",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": "Vector",
            "SupportQuantity": "Positional"
          }
        },
        {
          "Name": "Spacecraft Velocity, Geocentric Equatorial Inertial Coordinates",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "vel_gei",
          "Description": "Spacecraft Velocity, Geocentric Equatorial Inertial, GEI, Coordinates",
          "Caveats": "FAST Spacecraft Velocity in Geocentric Equatorial Inertial Coordinates",
          "Cadence": "PT1S",
          "Units": "km/s",
          "UnitsConversion": "1.0e3>m/s",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "GEI"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "vel_gei",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "vel_gei_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "km/s",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "vel_gei_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "km/s",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "vel_gei_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "km/s",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-1.0e+08",
          "ValidMax": "1.0e+08",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": "Vector",
            "SupportQuantity": "Other"
          }
        },
        {
          "Name": "Model Magnetic Field Vector, Geocentric Equatorial Inertial Coordinates",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "B_model_gei",
          "Description": "Model Magnetic Field Vector, Geocentric Equatorial Inertial, GEI, Coordinates",
          "Caveats": "Model Magnetic Field, IGRF Version 11 at the Date of Acquisition, in Geocentric Equatorial Inertial Coordinates",
          "Cadence": "PT1S",
          "Units": "nT",
          "UnitsConversion": "1.0e-9>T",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "GEI"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "B_model_gei",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "B_model_gei_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "B_model_gei_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "B_model_gei_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-1.0e+08",
          "ValidMax": "1.0e+08",
          "FillValue": "-1.0e+31",
          "Field": {
            "Qualifier": "Vector",
            "FieldQuantity": "Magnetic"
          }
        },
        {
          "Name": "Spacecraft Position, Altitude",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "alt",
          "Description": "Spacecraft Position, Altitude, relative to 6378.14 km",
          "Caveats": "FAST Altitude with respect to Earth Equatorial Radius, 6378.14 km, not mean Radius or Geodetic Altitude",
          "Cadence": "PT1S",
          "Units": "km",
          "UnitsConversion": "1.0e3>m",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Spherical",
            "CoordinateSystemName": "GEO"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "Altitude",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "0.0",
          "ValidMax": "99999.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": [
              "Scalar",
              "Magnitude"
            ],
            "SupportQuantity": "Positional"
          }
        },
        {
          "Name": "Spacecraft Position, Geographic Latitude",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "lat",
          "Description": "Spacecraft Position, Geographic, GEO, Latitude",
          "Caveats": "FAST Geographic Latitude with respect to the Sphere with Earth Equatorial Radius, 6378.14 km, not Geodetic",
          "Cadence": "PT1S",
          "Units": "°",
          "UnitsConversion": "0.0174532925>rad",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Spherical",
            "CoordinateSystemName": "GEO"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "Latitude",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "-90.0",
          "ValidMax": "90.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": [
              "Scalar",
              "DirectionAngle.ElevationAngle"
            ],
            "SupportQuantity": "Positional"
          }
        },
        {
          "Name": "Spacecraft Position, Geographic Latitude, as Audio",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "lat_audio",
          "Description": "Spacecraft Position, Geographic, GEO, Latitude, as Audio, do not use",
          "Caveats": "This parameter is virtual. It is calculated by calling the function ALTERNATE_VIEW with the following input parameters: lat.",
          "Cadence": "PT1S",
          "Units": "°",
          "UnitsConversion": "0.0174532925>rad",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Spherical",
            "CoordinateSystemName": "GEO"
          },
          "RenderingHints": {
            "AxisLabel": "Latitude",
            "ValueFormat": "E12.2",
            "ScaleMin": "-90.0",
            "ScaleMax": "90.0",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "-90.0",
          "ValidMax": "90.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": [
              "Scalar",
              "DirectionAngle.ElevationAngle"
            ],
            "SupportQuantity": "Positional"
          }
        },
        {
          "Name": "Spacecraft Position, Geographic Longitude",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "lng",
          "Description": "Spacecraft Position, Geographic, GEO, Longitude",
          "Caveats": "FAST Geographic Longitude with respect to the Sphere with Earth Equatorial Radius, 6378.14 km, not Geodetic",
          "Cadence": "PT1S",
          "Units": "°",
          "UnitsConversion": "0.0174532925>rad",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Spherical",
            "CoordinateSystemName": "GEO"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "Longitude",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "-180.0",
          "ValidMax": "180.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": [
              "Scalar",
              "DirectionAngle.AzimuthAngle"
            ],
            "SupportQuantity": "Positional"
          }
        },
        {
          "Name": "Spacecraft Position, Geographic Longitude, as Audio",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "lng_audio",
          "Description": "Spacecraft Position, Geographic, GEO, Longitude, as Audio, do not use",
          "Caveats": "This parameter is virtual. It is calculated by calling the function ALTERNATE_VIEW with the following input parameters: lng.",
          "Cadence": "PT1S",
          "Units": "°",
          "UnitsConversion": "0.0174532925>rad",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Spherical",
            "CoordinateSystemName": "GEO"
          },
          "RenderingHints": {
            "AxisLabel": "Longitude",
            "ValueFormat": "E12.2",
            "ScaleMin": "-180.0",
            "ScaleMax": "180.0",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "-180.0",
          "ValidMax": "180.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": [
              "Scalar",
              "DirectionAngle.AzimuthAngle"
            ],
            "SupportQuantity": "Positional"
          }
        },
        {
          "Name": "Spacecraft Position, Invariant Latitude",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "ilat",
          "Description": "Spacecraft Position, Invariant Latitude, tilted Dipole Coordinates",
          "Caveats": "FAST Invariant Latitude, ILAT, calculated with respect to the Offset, Tilted Dipole. Dipole Geographic Position: [-402.199, 287.504, 195.908] km, Dipole Orientation: Latitude 79.3637°, Longitude 288.454°. Invariant Latitude defined using 6371.2 km Radius with respect to Dipole Origin.",
          "Cadence": "PT1S",
          "Units": "°",
          "UnitsConversion": "0.0174532925>rad",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Spherical",
            "CoordinateSystemName": "CGM"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "ILAT",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "-90.0",
          "ValidMax": "90.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": [
              "Scalar",
              "DirectionAngle.ElevationAngle"
            ],
            "SupportQuantity": "Positional"
          }
        },
        {
          "Name": "Spacecraft Position, Invariant Longitude",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "ilng",
          "Description": "Spacecraft Position, Invariant Longitude, tilted Dipole Coordinates",
          "Caveats": "FAST Invariant Longitude, ILNG, calculated with respect to the Offset, Tilted Dipole. Dipole Geographic Position: [-402.199, 287.504, 195.908] km, Dipole Orientation: Latitude 79.3637°, Longitude 288.454°.",
          "Cadence": "PT1S",
          "Units": "°",
          "UnitsConversion": "0.0174532925>rad",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Spherical",
            "CoordinateSystemName": "CGM"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "ILNG",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "-180.0",
          "ValidMax": "180.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": [
              "Scalar",
              "DirectionAngle.AzimuthAngle"
            ],
            "SupportQuantity": "Positional"
          }
        },
        {
          "Name": "Spacecraft Position, Magnetic Local Time",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "mlt",
          "Description": "Spacecraft Position, Magnetic Local Time, MLT",
          "Caveats": "FAST Magnetic Local Time, MLT, calculated from the Invariant Longitude, ILNG, which in turn is derived by using an Offset, Tilted Dipole. Dipole Geographic Position: [-402.199, 287.504, 195.908] km, Dipole Orientation: Latitude 79.3637°, Longitude 288.454°.",
          "Cadence": "PT1S",
          "Units": "h",
          "UnitsConversion": "3600>s",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Spherical",
            "CoordinateSystemName": "CGM"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "MLT",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "0.0",
          "ValidMax": "24.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": [
              "Scalar",
              "DirectionAngle.AzimuthAngle"
            ],
            "SupportQuantity": "Positional"
          }
        },
        {
          "Name": "Spacecraft Footpoint, Geodetic Latitude",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "flat",
          "Description": "Spacecraft Footpoint, Geodetic Latitude, at 100 km Altitude",
          "Caveats": "Latitude of the FAST Spacecraft Magnetic Footpoint at 100 km Altitude, Geodetic Coordinates. IGRF Version 7 used for Magnetic Field Model (IGRF Version 7 is the default in the Field Line tracing Code). Latitude is in Geodetic Coordinates.",
          "Cadence": "PT1S",
          "Units": "°",
          "UnitsConversion": "0.0174532925>rad",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Spherical",
            "CoordinateSystemName": "WGS84"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "FLAT",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "-90.0",
          "ValidMax": "90.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": [
              "Scalar",
              "DirectionAngle.ElevationAngle"
            ],
            "SupportQuantity": "Positional"
          }
        },
        {
          "Name": "Spacecraft Footpoint, Geodetic Longitude",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "flng",
          "Description": "Spacecraft Footpoint, Geodetic Longitude, at 100 km Altitude",
          "Caveats": "Longitude of the FAST Spacecraft Magnetic Footpoint at 100 km Altitude, Geodetic Coordinates. IGRF Version 7 used for Magnetic Field Model (IGRF Version 7 is the default in the Field Line tracing Code). Longitude is in Geodetic Coordinates.",
          "Cadence": "PT1S",
          "Units": "°",
          "UnitsConversion": "0.0174532925>rad",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Spherical",
            "CoordinateSystemName": "WGS84"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "FLNG",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "-180.0",
          "ValidMax": "180.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": [
              "Scalar",
              "DirectionAngle.AzimuthAngle"
            ],
            "SupportQuantity": "Positional"
          }
        },
        {
          "Name": "Spacecraft Footpoint Magnetic Field, Geocentric Equatorial Inertial Coordinates",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "B_foot_gei",
          "Description": "Spacecraft Footpoint Magnetic Field, Geocentric Equatorial Inertial, GEI, Coordinates",
          "Caveats": "IGRF Version 7 Model Magnetic Field at the Position specified by FLAT, FLNG, and 100 km Altitude Geodetic (IGRF Version 7 is the default in the Field Line tracing Code)",
          "Cadence": "PT1S",
          "Units": "nT",
          "UnitsConversion": "1.0e-9>T",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "GEI"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "B_foot_gei",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "B_foot_gei_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "B_foot_gei_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "B_foot_gei_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-1.0e+08",
          "ValidMax": "1.0e+08",
          "FillValue": "-1.0e+31",
          "Field": {
            "Qualifier": "Vector",
            "FieldQuantity": "Magnetic"
          }
        },
        {
          "Name": "Sun Direction, Geocentric Equatorial Inertial Coordinates",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "sun_dir_gei",
          "Description": "Sun Direction Unit Vector, Geocentric Equatorial Inertial, GEI, Coordinates",
          "Caveats": "The Unit Vector pointing to the Sun Direction is used to construct the despun Spacecraft to Geocentric Equatorial Inertial Coordinate Transformation. This Unit Vector is also used to generate the GEI to Solar Magnetic Coordinate Transformation.",
          "Cadence": "PT1S",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "GEI"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "sun_dir_gei",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "sun_dir_gei_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "sun_dir_gei_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "sun_dir_gei_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-1.0",
          "ValidMax": "1.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": "Vector",
            "SupportQuantity": "Positional"
          }
        },
        {
          "Name": "Dipole Orientation, Geocentric Equatorial Inertial Coordinates",
          "Set": "Time Series defined by using: EPHEMERIS_EPOCH",
          "ParameterKey": "dip_orient_gei",
          "Description": "Dipole Orientation Unit Vector, Geocentric Equatorial Inertial, GEI, Coordinates",
          "Caveats": "Unit Vector giving Dipole Orientation in Geocentric Equatorial Inertial Coordinates. Dipole specified by the g10, g11, and h11 Values of the IGRF 11 Model, using the center Time of the Orbit as the Reference Epoch. Used to generate GEI to Solar Magnetic Coodinate Transformation.",
          "Cadence": "PT1S",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "GEI"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "dip_orient_gei",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "dip_orient_gei_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "dip_orient_gei_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "dip_orient_gei_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-1.0",
          "ValidMax": "1.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": "Vector",
            "SupportQuantity": "Positional"
          }
        },
        {
          "Name": "Reference Epoch Time for constant Orbit Variables",
          "ParameterKey": "Orbit_Fixed_Epoch",
          "Description": "Reference Epoch Time for Variables that are constant over the Orbit",
          "Caveats": "Time is specified as a TT2000 Variable. Conversion to TT2000 assumes the UTC as given by the FAST Data Decommutator is correct. Orbit_Fixed_Epoch specified as the median Time of the Ephemeris_Epoch Time Span. This Parameter exhibits an increasing Monotonic Progression.",
          "Cadence": "PT135M",
          "Units": "ns",
          "UnitsConversion": "1.0e-9>s",
          "RenderingHints": {
            "AxisLabel": "Orbit_Fixed_Epoch",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "1990-01-01T00:00:00.000000000",
          "ValidMax": "2030-01-01T00:00:00.999999999",
          "FillValue": "9999-12-31T23:59:59.999999999",
          "Support": {
            "SupportQuantity": "Temporal"
          }
        },
        {
          "Name": "Orbit Number",
          "Set": "Time Series defined by using: ORBIT_FIXED_EPOCH",
          "ParameterKey": "Orbit_Value",
          "Description": "Spacecraft Orbit Number",
          "Caveats": "Fixed Value of the Orbit Number, specified at the Orbit_Fixed_Epoch Time",
          "Cadence": "PT135M",
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "Orbit",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "0.0",
          "ValidMax": "99999.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": "Scalar",
            "SupportQuantity": "Other"
          }
        },
        {
          "Name": "Magnetometer Coupling Matrix Components",
          "Set": "Time Series defined by using: ORBIT_FIXED_EPOCH",
          "ParameterKey": "Coupling_Matrix",
          "Description": "Magnetometer Coupling Matrix Components",
          "Caveats": "Magnetometer Coupling Matrix Components, fixed Values for the Orbit. Coupling Matrix Components can change from Orbit to Orbit.",
          "Cadence": "PT135M",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "SC"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "Coupling_Matrix",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "9",
            "Element": [
              {
                "Name": "sigma_xx",
                "Index": "1",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "sigma_xy",
                "Index": "2",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "sigma_xz",
                "Index": "3",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              },
              {
                "Name": "sigma_yx",
                "Index": "4",
                "RenderingHints": {
                  "AxisLabel": "4"
                }
              },
              {
                "Name": "sigma_yy",
                "Index": "5",
                "RenderingHints": {
                  "AxisLabel": "5"
                }
              },
              {
                "Name": "sigma_yz",
                "Index": "6",
                "RenderingHints": {
                  "AxisLabel": "6"
                }
              },
              {
                "Name": "sigma_zx",
                "Index": "7",
                "RenderingHints": {
                  "AxisLabel": "7"
                }
              },
              {
                "Name": "sigma_zy",
                "Index": "8",
                "RenderingHints": {
                  "AxisLabel": "8"
                }
              },
              {
                "Name": "sigma_zz",
                "Index": "9",
                "RenderingHints": {
                  "AxisLabel": "9"
                }
              }
            ]
          },
          "ValidMin": "-2.0",
          "ValidMax": "2.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": "Tensor",
            "SupportQuantity": "Other"
          }
        },
        {
          "Name": "Magnetometer Offsets",
          "Set": "Time Series defined by using: ORBIT_FIXED_EPOCH",
          "ParameterKey": "Offsets",
          "Description": "Magnetometer Sensor Component Offsets",
          "Caveats": "Magnetometer Sensor Component Offsets, fixed Values for the Orbit. Offsets can change from Orbit to Orbit.",
          "Cadence": "PT135M",
          "Units": "nT",
          "UnitsConversion": "1.0e-9>T",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Cartesian",
            "CoordinateSystemName": "SC"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "Offsets",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "3",
            "Element": [
              {
                "Name": "o_x",
                "Qualifier": "Component.I",
                "Index": "1",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "o_y",
                "Qualifier": "Component.J",
                "Index": "2",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "o_z",
                "Qualifier": "Component.K",
                "Index": "3",
                "Units": "nT",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              }
            ]
          },
          "ValidMin": "-1000.0",
          "ValidMax": "1000.0",
          "FillValue": "-1.0e+31",
          "Field": {
            "Qualifier": "Vector",
            "FieldQuantity": "Magnetic"
          }
        },
        {
          "Name": "Spin Axis Orientation",
          "Set": "Time Series defined by using: ORBIT_FIXED_EPOCH",
          "ParameterKey": "Spin_Axis",
          "Description": "Spin Axis Orientation, Right Ascension and Declination",
          "Caveats": "Spin Axis Right Ascension, RA, and Declination, DEC, obtained by comparing IGRF Model Field with Data. The Parameters RA_FDF and DEC_FDF are the starting Values for the initial Comparison where FDF standing for Flight Dynamics Facility.",
          "Cadence": "PT135M",
          "Units": "°",
          "UnitsConversion": "0.0174532925>rad",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Spherical",
            "CoordinateSystemName": "GEI"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "Spin_Axis",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "Structure": {
            "Size": "4",
            "Element": [
              {
                "Name": "RA",
                "Index": "1",
                "Units": "°",
                "RenderingHints": {
                  "AxisLabel": "1"
                }
              },
              {
                "Name": "DEC",
                "Index": "2",
                "Units": "°",
                "RenderingHints": {
                  "AxisLabel": "2"
                }
              },
              {
                "Name": "RA_FDF",
                "Index": "3",
                "Units": "°",
                "RenderingHints": {
                  "AxisLabel": "3"
                }
              },
              {
                "Name": "DEC_FDF",
                "Index": "4",
                "Units": "°",
                "RenderingHints": {
                  "AxisLabel": "4"
                }
              }
            ]
          },
          "ValidMin": "-720.0",
          "ValidMax": "720.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": [
              "Scalar",
              "DirectionAngle.AzimuthAngle",
              "DirectionAngle.ElevationAngle"
            ],
            "SupportQuantity": "Other"
          }
        },
        {
          "Name": "Spin Phase Delta",
          "Set": "Time Series defined by using: ORBIT_FIXED_EPOCH",
          "ParameterKey": "Spin_Phase_Delta",
          "Description": "Spin Phase Delta in the Spin Plane",
          "Caveats": "Angle by which the measured Field leads the Model Field in the Spin Plane, before correction. The Correction is used to rotate the measured Field back by this Angle.",
          "Cadence": "PT135M",
          "Units": "°",
          "UnitsConversion": "0.0174532925>rad",
          "CoordinateSystem": {
            "CoordinateRepresentation": "Spherical",
            "CoordinateSystemName": "GEI"
          },
          "RenderingHints": {
            "DisplayType": "TimeSeries",
            "AxisLabel": "Spin_Phase_Delta",
            "ValueFormat": "E12.2",
            "ScaleType": "LinearScale"
          },
          "ValidMin": "-720.0",
          "ValidMax": "720.0",
          "FillValue": "-1.0e+31",
          "Support": {
            "Qualifier": [
              "Scalar",
              "DirectionAngle.AzimuthAngle"
            ],
            "SupportQuantity": "Other"
          }
        }
      ]
    }
  }
}