2.3.2 spase://NASA/NumericalData/THEMIS/E/Ephemeris/SSCWeb/PT1M THEMIS-E (P4) Orbit (Ephemeris) 2021-04-27T15:38:11Z THEMIS-E Orbital Information provided via the Satellite Situation Center, SSCWeb, System and Services, Space Physics Data Facility, SPDF, GSFC, NASA V. Angelopoulos spase://SMWG/Person/Vassilis.Angelopoulos PrincipalInvestigator spase://SMWG/Person/Robert.E.McGuire MetadataContact spase://SMWG/Person/Lee.Frost.Bargatze MetadataContact Satellite Situation Center, SSCWeb, System and Services https://sscweb.gsfc.nasa.gov The Satellite Situation Center Web, SSCWeb, Service has been developed and is operated jointly by the NASA/GSFC Space Physics Data Facility, SPDF, and the National Space Science Data Center, NSSDC, to support a Range of NASA Science Programs and to fulfill Key International NASA Responsibilities including those of NSSDC and the World Data Center-A for Rockets and Satellites. The Software and associated Database of SSCWeb together form a System to cast Geocentric Spacecraft Location Information into a Framework of Empirical Geophysical Regions and Mappings of Spacecraft Locations along Lines of the Earth's Magnetic Field. This Capability is one Key to Mission Science Planning, both Single Missions and Coordinated Observations of Multiple Spacecraft with Ground-Based Investigations, and to subsequent Multi-Mission Data Analysis. spase://VSPO/NumericalData/THEMIS/E/Ephemeris/SSCWeb/PT1M spase://SMWG/Repository/NASA/GSFC/SPDF Online Open FTPS from SPDF (not with most browsers) ftps://spdf.gsfc.nasa.gov/pub/data/themis/the/ssc/ Access to Data in CDF Format via ftp from SPDF HTTPS from SPDF https://spdf.gsfc.nasa.gov/pub/data/themis/the/ssc/ Access to Data in CDF Format via http from SPDF CDAWeb https://cdaweb.gsfc.nasa.gov/cgi-bin/eval2.cgi?dataset=THE_OR_SSC&index=sp_phys THE_OR_SSC Access to ASCII, CDF, and plots via NASA/GSFC CDAWeb CDF None V. Angelopoulos. Please acknowledge the data providers and CDAWeb when using these data. spase://SMWG/Repository/NASA/GSFC/SPDF Online Open CDAWeb HAPI Server https://cdaweb.gsfc.nasa.gov/hapi THE_OR_SSC Web Service to this product using the HAPI interface. CSV V. Angelopoulos. Please acknowledge the data providers and CDAWeb when using these data. Calibrated spase://SMWG/Instrument/THEMIS/E/Ephemeris Ephemeris 2007-02-18T00:14:00 2017-05-01T23:59:59.999 PT1M Epoch Time, Orbit Epoch Epoch Time, Orbit This parameter exhibits an increasing monotonic progression. PT1M ms 1.0e-3>s Epoch 6.1725348219904e+13 6.5733185019904e+13 01-Jan-1956 00:00:00.000 01-Jan-2083 00:00:00.000 31-Dec-9999 23:59:59.999 Temporal Spacecraft Position, Orbital Radius Time series defined by using: EPOCH RADIUS Spacecraft Position, Orbital Radius PT1M Re 6,3712e6>m TimeSeries RADIUS F8.2 0.0 10000.0 0.0 10000.0 -1.0e+31 Vector Positional Spacecraft Position Vector, GSE, Cartesian, Time Series Time series defined by using: EPOCH XYZ_GSE Spacecraft Position Vector, Geocentric Solar Ecliptic, GSE, Cartesian Components, Time Series . PT1M Re 6,3712e6>m Cartesian GSE TimeSeries F8.2 -10000.0 10000.0 3 x 1 x y 2 y z 3 z -10000.0 10000.0 -1.0e+31 Vector Positional Spacecraft Position Vector, GSE, Cartesian, Orbit Time series defined by using: EPOCH XYZ_GSEO Spacecraft Position Vector, Geocentric Solar Ecliptic, GSE, Cartesian Components, Orbit . This parameter is virtual. It is calculated by calling the function ALTERNATE_VIEW with the following input parameters: XYZ_GSE. PT1M Re 6,3712e6>m Cartesian GSE F8.2 -10000.0 10000.0 3 x 1 x y 2 y z 3 z -10000.0 10000.0 -1.0e+31 Vector Positional Spacecraft Position, GSE, Latitude Time series defined by using: EPOCH GSE_LAT Spacecraft Position, Geocentric Solar Ecliptic, GSE, Spherical Coordinates, Latitude PT1M ° 0.0174532925>rad Spherical GSE TimeSeries GSE_LAT F8.2 -90.0 90.0 -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Positional Spacecraft Position, GSE, Longitude Time series defined by using: EPOCH GSE_LON Spacecraft Position, Geocentric Solar Ecliptic, GSE, Spherical Coordinates, Longitude PT1M ° 0.0174532925>rad Spherical GSE TimeSeries GSE_LON F8.2 0.0 360.0 0.0 360.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Spacecraft Position, GSE, Local Time Time series defined by using: EPOCH GSE_LCT_T Spacecraft Position, Geocentric Solar Ecliptic, GSE, Local Time PT1M h 3600>s Spherical GSE TimeSeries GSE_LCT_T F8.2 0.0 24.0 0.0 24.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Spacecraft Position Vector, GSM, Cartesian, Time Series Time series defined by using: EPOCH XYZ_GSM Spacecraft Position Vector, Geocentric Solar Magnetospheric, GSM, Cartesian Components, Time Series . PT1M Re 6,3712e6>m Cartesian GSM TimeSeries F8.2 -10000.0 10000.0 3 x 1 x y 2 y z 3 z -10000.0 10000.0 -1.0e+31 Vector Positional Spacecraft Position Vector, GSM, Cartesian, Orbit Time series defined by using: EPOCH XYZ_GSMO Spacecraft Position Vector, Geocentric Solar Magnetospheric, GSM, Cartesian Components, Orbit . This parameter is virtual. It is calculated by calling the function ALTERNATE_VIEW with the following input parameters: XYZ_GSM. PT1M Re 6,3712e6>m Cartesian GSM F8.2 -10000.0 10000.0 3 x 1 x y 2 y z 3 z -10000.0 10000.0 -1.0e+31 Vector Positional Spacecraft Position, GSM, Latitude Time series defined by using: EPOCH GSM_LAT Spacecraft Position, Geocentric Solar Magnetospheric, GSM, Spherical Coordinates, Latitude PT1M ° 0.0174532925>rad Spherical GSM TimeSeries GSM_LAT F8.2 -90.0 90.0 -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Positional Spacecraft Position, GSM, Longitude Time series defined by using: EPOCH GSM_LON Spacecraft Position, Geocentric Solar Magnetospheric, GSM, Spherical Coordinates, Longitude PT1M ° 0.0174532925>rad Spherical GSM TimeSeries GSM_LON F8.2 0.0 360.0 0.0 360.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Spacecraft Position Vector, SM, Cartesian, Time Series Time series defined by using: EPOCH XYZ_SM Spacecraft Position Vector, Solar Magnetospheric, SM, Cartesian Components, Time Series . PT1M Re 6,3712e6>m Cartesian SM TimeSeries F8.2 -10000.0 10000.0 3 x 1 x y 2 y z 3 z -10000.0 10000.0 -1.0e+31 Vector Positional Spacecraft Position Vector, SM, Cartesian, Orbit Time series defined by using: EPOCH XYZ_SMO Spacecraft Position Vector, Solar Magnetospheric, SM, Cartesian Components, Orbit . This parameter is virtual. It is calculated by calling the function ALTERNATE_VIEW with the following input parameters: XYZ_SM. PT1M Re 6,3712e6>m Cartesian SM F8.2 -10000.0 10000.0 3 x 1 x y 2 y z 3 z -10000.0 10000.0 -1.0e+31 Vector Positional Spacecraft Position, SM, Latitude Time series defined by using: EPOCH SM_LAT Spacecraft Position, Solar Magnetospheric, SM, Spherical Coordinates, Latitude PT1M ° 0.0174532925>rad Spherical SM TimeSeries SM_LAT F8.2 -90.0 90.0 -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Positional Spacecraft Position, SM, Longitude Time series defined by using: EPOCH SM_LON Spacecraft Position, Solar Magnetospheric, SM, Spherical Coordinates, Longitude PT1M ° 0.0174532925>rad Spherical SM TimeSeries SM_LON F8.2 0.0 360.0 0.0 360.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Spacecraft Position, SM, Local Time Time series defined by using: EPOCH SM_LCT_T Spacecraft Position, Solar Magnetospheric, SM, Local Time PT1M h 3600>s Spherical SM TimeSeries SM_LCT_T F8.2 0.0 24.0 0.0 24.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Spacecraft Position Vector, GEO, Cartesian, Time Series Time series defined by using: EPOCH XYZ_GEO Spacecraft Position Vector, Geographic, GEO, Cartesian Components, Time Series . PT1M Re 6,3712e6>m Cartesian GEO TimeSeries F8.2 -10000.0 10000.0 3 x 1 x y 2 y z 3 z -10000.0 10000.0 -1.0e+31 Vector Positional Spacecraft Position Vector, GEO, Cartesian, Orbit Time series defined by using: EPOCH XYZ_GEOO Spacecraft Position Vector, Geographic, GEO, Cartesian Components, Orbit . This parameter is virtual. It is calculated by calling the function ALTERNATE_VIEW with the following input parameters: XYZ_GEO. PT1M Re 6,3712e6>m Cartesian GEO F8.2 -10000.0 10000.0 3 x 1 x y 2 y z 3 z -10000.0 10000.0 -1.0e+31 Vector Positional Spacecraft Position, GEO, Latitude Time series defined by using: EPOCH GEO_LAT Spacecraft Position, Geographic, GEO, Spherical Coordinates, Latitude PT1M ° 0.0174532925>rad Spherical GEO TimeSeries GEO_LAT F8.2 -90.0 90.0 -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Positional Spacecraft Position, GEO, Longitude Time series defined by using: EPOCH GEO_LON Spacecraft Position, Geographic, GEO, Spherical Coordinates, Longitude PT1M ° 0.0174532925>rad Spherical GEO TimeSeries GEO_LON F8.2 0.0 360.0 0.0 360.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Spacecraft Position, GEO, Local Time Time series defined by using: EPOCH GEO_LCT_T Spacecraft Position, Geographic, GEO, Local Time PT1M h 3600>s Spherical GEO TimeSeries GEO_LCT_T F8.2 0.0 24.0 0.0 24.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Spacecraft Footpoint, GEO, Latitude, North Time series defined by using: EPOCH NorthBtrace_GEO_LAT Spacecraft Footpoint, 100 km Altitude, Geographic, GEO, Spherical Coordinates, Latitude, Northern Hemisphere PT1M ° 0.0174532925>rad Spherical GEO TimeSeries NorthBtrace_GEO_LAT F8.2 -90.0 90.0 -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Positional Spacecraft Footpoint, GEO, Longitude, North Time series defined by using: EPOCH NorthBtrace_GEO_LON Spacecraft Footpoint, 100 km Altitude, Geographic, GEO, Spherical Coordinates, Longitude, Northern Hemisphere PT1M ° 0.0174532925>rad Spherical GEO TimeSeries NorthBtrace_GEO_LON F8.2 0.0 360.0 0.0 360.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Spacecraft Position-Footpoint Arc Length, GEO, Latitude, North Time series defined by using: EPOCH NorthBtrace_GEO_ARCLEN Spacecraft Position to Footpoint, 100 km Altitude, Arc Length, Geographic, GEO, Coordinates, Northern Hemisphere PT1M Re 6,3712e6>m Spherical GEO TimeSeries NorthBtrace_GEO_ARCLEN F8.2 0.0 400.0 0.0 400.0 -1.0e+31 Magnitude Positional Spacecraft Footpoint, GEO, Latitude, South Time series defined by using: EPOCH SouthBtrace_GEO_LAT Spacecraft Footpoint, 100 km Altitude, Geographic, GEO, Spherical Coordinates, Latitude, Southern Hemisphere PT1M ° 0.0174532925>rad Spherical GEO TimeSeries SouthBtrace_GEO_LAT F8.2 -90.0 90.0 -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Positional Spacecraft Footpoint, GEO, Longitude, South Time series defined by using: EPOCH SouthBtrace_GEO_LON Spacecraft Footpoint, 100 km Altitude, Geographic, GEO, Spherical Coordinates, Longitude, Southern Hemisphere PT1M ° 0.0174532925>rad Spherical GEO TimeSeries SouthBtrace_GEO_LON F8.2 0.0 360.0 0.0 360.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Spacecraft Position-Footpoint Arc Length, GEO, Latitude, South Time series defined by using: EPOCH SouthBtrace_GEO_ARCLEN Spacecraft Position to Footpoint, 100 km Altitude, Arc Length, Geographic, GEO, Coordinates, Southern Hemisphere PT1M Re 6,3712e6>m Spherical GEO TimeSeries SouthBtrace_GEO_ARCLEN F8.2 0.0 400.0 0.0 400.0 -1.0e+31 Magnitude Positional Spacecraft Position Vector, MAG, Cartesian, Time Series Time series defined by using: EPOCH XYZ_GM Spacecraft Position Vector, Geomagnetic, MAG, Cartesian Components, Time Series . PT1M Re 6,3712e6>m Cartesian MAG TimeSeries F8.2 -10000.0 10000.0 3 x 1 x y 2 y z 3 z -10000.0 10000.0 -1.0e+31 Vector Positional Spacecraft Position Vector, MAG, Cartesian, Orbit Time series defined by using: EPOCH XYZ_GMO Spacecraft Position Vector, Geomagnetic, MAG, Cartesian Components, Orbit . This parameter is virtual. It is calculated by calling the function ALTERNATE_VIEW with the following input parameters: XYZ_GM. PT1M Re 6,3712e6>m Cartesian MAG F8.2 -10000.0 10000.0 3 x 1 x y 2 y z 3 z -10000.0 10000.0 -1.0e+31 Vector Positional Spacecraft Position, MAG, Latitude Time series defined by using: EPOCH GM_LAT Spacecraft Position, Geomagnetic, MAG, Spherical Coordinates, Latitude PT1M ° 0.0174532925>rad Spherical MAG TimeSeries GM_LAT F8.2 -90.0 90.0 -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Positional Spacecraft Position, MAG, Longitude Time series defined by using: EPOCH GM_LON Spacecraft Position, Geomagnetic, MAG, Spherical Coordinates, Longitude PT1M ° 0.0174532925>rad Spherical MAG TimeSeries GM_LON F8.2 0.0 360.0 0.0 360.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Spacecraft Position, MAG, Local Time Time series defined by using: EPOCH GM_LCT_T Spacecraft Position, Geomagnetic, MAG, Local Time PT1M h 3600>s Spherical MAG TimeSeries GM_LCT_T F8.2 0.0 24.0 0.0 24.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Spacecraft Footpoint, MAG, Latitude, North Time series defined by using: EPOCH NorthBtrace_GM_LAT Spacecraft Footpoint, 100 km Altitude, Geomagnetic, MAG, Spherical Coordinates, Latitude, Northern Hemisphere PT1M ° 0.0174532925>rad Spherical MAG TimeSeries NorthBtrace_GM_LAT F8.2 -90.0 90.0 -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Positional Spacecraft Footpoint, MAG, Longitude, North Time series defined by using: EPOCH NorthBtrace_GM_LON Spacecraft Footpoint, 100 km Altitude, Geomagnetic, MAG, Spherical Coordinates, Longitude, Northern Hemisphere PT1M ° 0.0174532925>rad Spherical MAG TimeSeries NorthBtrace_GM_LON F8.2 0.0 360.0 0.0 360.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Spacecraft Position-Footpoint Arc Length, MAG, Latitude, North Time series defined by using: EPOCH NorthBtrace_GM_ARCLEN Spacecraft Position to Footpoint, 100 km Altitude, Arc Length, Geomagnetic, MAG, Coordinates, Northern Hemisphere PT1M Re 6,3712e6>m Spherical MAG TimeSeries NorthBtrace_GM_ARCLEN F8.2 0.0 400.0 0.0 400.0 -1.0e+31 Magnitude Positional Spacecraft Footpoint, MAG, Latitude, South Time series defined by using: EPOCH SouthBtrace_GM_LAT Spacecraft Footpoint, 100 km Altitude, Geomagnetic, MAG, Spherical Coordinates, Latitude, Southern Hemisphere PT1M ° 0.0174532925>rad Spherical MAG TimeSeries SouthBtrace_GM_LAT F8.2 -90.0 90.0 -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Positional Spacecraft Footpoint, MAG, Longitude, South Time series defined by using: EPOCH SouthBtrace_GM_LON Spacecraft Footpoint, 100 km Altitude, Geomagnetic, MAG, Spherical Coordinates, Longitude, Southern Hemisphere PT1M ° 0.0174532925>rad Spherical MAG TimeSeries SouthBtrace_GM_LON F8.2 0.0 360.0 0.0 360.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Spacecraft Position-Footpoint Arc Length, MAG, Latitude, South Time series defined by using: EPOCH SouthBtrace_GM_ARCLEN Spacecraft Position to Footpoint, 100 km Altitude, Arc Length, Geomagnetic, MAG, Coordinates, Southern Hemisphere PT1M Re 6,3712e6>m Spherical MAG TimeSeries SouthBtrace_GM_ARCLEN F8.2 0.0 400.0 0.0 400.0 -1.0e+31 Magnitude Positional Total Magnetic Field Strength, Tsyganenko 95 Time series defined by using: EPOCH MAG_STRTH Total Magnetic Field Strength, Tsyganenko 95 Model PT1M nT 1e-9>T TimeSeries Magnetic Strength F8.2 0.0 60000.0 0.0 60000.0 -1.0e+31 Magnitude Magnetic Spacecraft Position-Neutral Sheet Distance, Tsyganenko 95 Time series defined by using: EPOCH DNEUTS Spacecraft Position-Neutral Sheet Distance, Tsyganenko 95 Model PT1M Re 6,3712e6>m TimeSeries Dist from T95 NS F8.2 -40.0 40.0 -40.0 40.0 -1.0e+31 Magnitude Positional Spacecraft Position-Bow Shock Distance, Tsyganenko 95 Time series defined by using: EPOCH BOW_SHOCK Spacecraft Position-Bow Shock Distance, Tsyganenko 95 Model PT1M Re 6,3712e6>m TimeSeries Dist from P93 Bow Shock F8.2 -200.0 200.0 -200.0 200.0 -1.0e+31 Magnitude Positional Spacecraft Position-Magnetopause Distance, Tsyganenko 95 Time series defined by using: EPOCH MAG_PAUSE Spacecraft Position-Magnetopause Distance, Tsyganenko 95 Model PT1M Re 6,3712e6>m TimeSeries Dist from Magnetopause F8.2 -30.0 200.0 -30.0 200.0 -1.0e+31 Magnitude Positional Spacecraft Position, L Shell Value Time series defined by using: EPOCH L_VALUE Spacecraft Position, L Shell Value PT1M TimeSeries L Value F8.2 1.0 400.0 1.0 400.0 -1.0e+31 Magnitude Positional Spacecraft Position, Invariant Latitude Time series defined by using: EPOCH INVAR_LAT Spacecraft Position, Invariant Latitude PT1M ° 0.0174532925>rad Spherical MAG TimeSeries INVAR_LAT F8.2 -90.0 90.0 -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Positional Magnetic Field, X Component, at the Spacecraft, Tsyganenko 89C Time series defined by using: EPOCH MAG_X Magnetic Field, X Component, at the Spacecraft estimated by using the Tsyganenko 89C Model PT1M nT 1e-9>T Cartesian MAG TimeSeries BGSE-X F8.2 -60000.0 60000.0 -60000.0 60000.0 -1.0e+31 Component.I Magnetic Magnetic Field, Y Component, at the Spacecraft, Tsyganenko 89C Time series defined by using: EPOCH MAG_Y Magnetic Field, Y Component, at the Spacecraft estimated by using the Tsyganenko 89C Model PT1M nT 1e-9>T Cartesian MAG TimeSeries BGSE-Y F8.2 -60000.0 60000.0 -60000.0 60000.0 -1.0e+31 Component.J Magnetic Magnetic Field, Z Component, at the Spacecraft, Tsyganenko 89C Time series defined by using: EPOCH MAG_Z Magnetic Field, Z Component, at the Spacecraft estimated by using the Tsyganenko 89C Model PT1M nT 1e-9>T Cartesian MAG TimeSeries BGSE-Z F8.2 -60000.0 60000.0 -60000.0 60000.0 -1.0e+31 Component.K Magnetic