2.3.0 spase://ESA/NumericalData/Cluster/Ephemeris/JP/PredictedGeometricPosition/PT5M Cluster Predicted Geometric Positions (PGP) Spacecraft Tetrahedron, JSOC Parameter (JP), 5 min Data 2021-04-27T17:52:14Z Cluster Predicted Geometric Positions generated by the Joint Science Operations Centre, JSOC. See M.A. Hapgood et al., The Joint Science Operations Centre, Space Sci. Rev., 79, 487-525, 1997. For Geometrical Configuration Parameters, see page 328 of Tetrahedron Geometric Factors by P. Robert et al., in Analysis Methods for Multi-Spacecraft Data, Editors G. Paschmann and P. Daly, published in 1998 by the European Space Agency, ESA, and the International Space Science Institute, ISSI, Bern. M.A. Hapgood. Refer to Cluster Science Data System, CSDS, for Rules of Acknowledgement spase://SMWG/Person/Michael.A.Hapgood PrincipalInvestigator spase://SMWG/Person/Robert.E.McGuire MetadataContact spase://SMWG/Person/Lee.Frost.Bargatze MetadataContact Cluster Science Archive, CSA, Web Page https://www.cosmos.esa.int/web/csa/ Web Page for access to High-Time Resolution Data from the Cluster and Double Star Missions Cluster Science Data System, CSDS, Web Page http://sci.esa.int/cluster/52770-csds/ The Cluster Science Working Team along with the ESA Cluster Project Team have established the Cluster Science Data System, CSDS, a distributed Set of Data Centres, most of which are associated with one or more of the Cluster Experiments. With Software provided by the Experiment Team, each Data Centre processes the Data and then exchanges them with all the other Centres to obtain a full Data Set in a standard Format. spase://ESA/NumericalData/Cluster/Ephemeris/JP/PGP/PT1M spase://VSPO/NumericalData/P_CLUSTER1_HDR_PGP_60S spase://VSPO/NumericalData/Cluster/Ephemeris/JP-PGP/PT1M spase://VSPO/NumericalData/Cluster/Ephemeris/JP/PGP/PT1M spase://SMWG/Repository/NASA/GSFC/SPDF Online Open FTPS from SPDF (not with most browsers) ftps://spdf.gsfc.nasa.gov/pub/data/cluster/cl/jp/pgp/ Access to Data in CDF Format via ftp from SPDF HTTPS from SPDF https://spdf.gsfc.nasa.gov/pub/data/cluster/cl/jp/pgp/ Access to Data in CDF Format via http from SPDF CDAWeb https://cdaweb.gsfc.nasa.gov/cgi-bin/eval2.cgi?dataset=CL_JP_PGP&index=sp_phys CL_JP_PGP Access to ASCII, CDF, and Plots via NASA/GSFC CDAWeb CDF None M.A. Hapgood. Refer to Cluster Science Data System, CSDS, for Rules of Acknowledgement. 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 CL_JP_PGP Web Service to this product using the HAPI interface. CSV M.A. Hapgood. Refer to Cluster Science Data System, CSDS, for Rules of Acknowledgement. Please acknowledge the Data Providers and CDAWeb when using these Data. Calibrated spase://SMWG/Instrument/Cluster/JSOC Ephemeris InstrumentStatus 2000-08-14T20:35:00.000 P3Y PT5M Earth.Magnetosphere Earth.Magnetosphere.Magnetotail Earth.Magnetosphere.Main Earth.Magnetosphere.RadiationBelt Earth.Magnetosheath Heliosphere.NearEarth JSOC Predicted Orbits, calculated by using Cluster-Samba, C3, as the Reference Spacecraft Half Interval Half_interval__CL_JP_PGP Half Interval, equal to Half of the Separation between Time Tags averaged of the over the File PT5M ms 1.0e-3>s Half Sample Time Interval -1.0e+31 Temporal Epoch Time Tags Epoch__CL_JP_PGP Epoch Time Tags, Spot Value Time Tags This Parameter exhibits an increasing Monotonic Progression. PT5M ms 1.0e-3>s Epoch 6.3145505019904e+13 6.3148183419904e+13 LinearScale 01-Jan-1994 00:00:00.000 01-Jan-2010 00:00:00.000 -1.0e+31 Temporal Spacecraft Orbit Number, including Phase Time Series defined by using: EPOCH__CL_JP_PGP sc_orbit_num__CL_JP_PGP Spacecraft Orbit Number, including Fractional Phase Part Average Type: standard PT5M 1.0>(orbit.phase) Fract Orbit E13.6 0.0 500.0 LinearScale 0.0 1000.0 -1.0e+31 Scalar Other Predicted Spacecraft Position Vector, Geocentric Solar Ecliptic Cartesian Coordinates, for the Reference Satellite Time Series defined by using: EPOCH__CL_JP_PGP sc_r_xyz_gse__CL_JP_PGP Predicted Spacecraft Position Vector, Geocentric Solar Ecliptic, GSE, Cartesian Coordinates, for the Reference Satellite Average Type: standard PT5M km 1.0e3>m Cartesian GSE E13.6 -150000.0 150000.0 LinearScale 3 x (GSE) pred 1 x (GSE) y (GSE) pred 2 y (GSE) z (GSE) pred 3 z (GSE) -140000.0 140000.0 -1.0e+31 Vector Positional Predicted Spacecraft Velocity Vector, Geocentric Solar Ecliptic Cartesian Coordinates, for the Reference Satellite Time Series defined by using: EPOCH__CL_JP_PGP sc_v_xyz_gse__CL_JP_PGP Predicted Spacecraft Velocity Vector, Geocentric Solar Ecliptic, GSE, Cartesian Coordinates, for the Reference Satellite Average Type: standard PT5M km/s 1.0e3>m/s Cartesian GSE E13.6 -10.0 10.0 LinearScale 3 Vx (GSE) pred 1 x (GSE) Vy (GSE) pred 2 y (GSE) Vz (GSE) pred 3 z (GSE) -10.0 10.0 -1.0e+31 Vector Positional Predicted Spacecraft 1, Cluster-Rumba, Position Vector, Geocentric Solar Ecliptic Cartesian Coordinates, with respect to the Reference Satellite Position Time Series defined by using: EPOCH__CL_JP_PGP sc_dr1_xyz_gse__CL_JP_PGP Predicted Spacecraft 1, Cluster-Rumba, Position Vector, Geocentric Solar Ecliptic, GSE, Cartesian Coordinates, with respect to the Reference Satellite Position Average Type: standard PT5M km 1.0e3>m Cartesian GSE E13.6 -20000.0 20000.0 LinearScale 3 C1 dx pred 1 x (GSE) C1 dy pred 2 y (GSE) C1 dz pred 3 z (GSE) -100000.0 100000.0 -1.0e+31 Vector Positional Predicted Spacecraft 2, Cluster-Salsa, Position Vector, Geocentric Solar Ecliptic Cartesian Coordinates, with respect to the Reference Satellite Position Time Series defined by using: EPOCH__CL_JP_PGP sc_dr2_xyz_gse__CL_JP_PGP Predicted Spacecraft 2, Cluster-Salsa, Position Vector, Geocentric Solar Ecliptic, GSE, Cartesian Coordinates, with respect to the Reference Satellite Position Average Type: standard PT5M km 1.0e3>m Cartesian GSE E13.6 -20000.0 20000.0 LinearScale 3 C2 dx pred 1 x (GSE) C2 dy pred 2 y (GSE) C2 dz pred 3 z (GSE) -100000.0 100000.0 -1.0e+31 Vector Positional Predicted Spacecraft 3, Cluster-Samba, Position Vector, Geocentric Solar Ecliptic Cartesian Coordinates, with respect to the Reference Satellite Position Time Series defined by using: EPOCH__CL_JP_PGP sc_dr3_xyz_gse__CL_JP_PGP Predicted Spacecraft 3, Cluster-Samba, Position Vector, Geocentric Solar Ecliptic, GSE, Cartesian Coordinates, with respect to the Reference Satellite Position Average Type: standard PT5M km 1.0e3>m Cartesian GSE E13.6 -20000.0 20000.0 LinearScale 3 C3 dx pred 1 x (GSE) C3 dy pred 2 y (GSE) C3 dz pred 3 z (GSE) -100000.0 100000.0 -1.0e+31 Vector Positional Predicted Spacecraft 4, Cluster-Tango, Position Vector, Geocentric Solar Ecliptic Cartesian Coordinates, with respect to the Reference Satellite Position Time Series defined by using: EPOCH__CL_JP_PGP sc_dr4_xyz_gse__CL_JP_PGP Predicted Spacecraft 4, Cluster-Tango, Position Vector, Geocentric Solar Ecliptic, GSE, Cartesian Coordinates, with respect to the Reference Satellite Position Average Type: standard PT5M km 1.0e3>m Cartesian GSE E13.6 -20000.0 20000.0 LinearScale 3 C4 dx pred 1 x (GSE) C4 dy pred 2 y (GSE) C4 dz pred 3 z (GSE) -100000.0 100000.0 -1.0e+31 Vector Positional Predicted Spacecraft 1, Cluster-Rumba, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic Spherical Coordinates Time Series defined by using: EPOCH__CL_JP_PGP sc_at1_lat__CL_JP_PGP Predicted Spacecraft 1, Cluster-Rumba, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates Average Type: angle_degrees PT5M ° 0.0174532925>rad Spherical GSE C1 Predicted Lat (GSE) E13.6 -90.0 90.0 LinearScale -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Scalar Positional Predicted Spacecraft 1, Cluster-Rumba, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic Spherical Coordinates Time Series defined by using: EPOCH__CL_JP_PGP sc_at1_long__CL_JP_PGP Predicted Spacecraft 1, Cluster-Rumba, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates, Angle from the X-axis in the GSE X-Y Plane Average Type: angle_degrees PT5M ° 0.0174532925>rad Spherical GSE C1 Predicted Long (GSE) E13.6 0.0 360.0 LinearScale 0.0 360.0 -1.0e+31 DirectionAngle.AzimuthAngle Scalar Positional Predicted Spacecraft 2, Cluster-Salsa, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic Spherical Coordinates Time Series defined by using: EPOCH__CL_JP_PGP sc_at2_lat__CL_JP_PGP Predicted Spacecraft 2, Cluster-Salsa, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates Average Type: angle_degrees PT5M ° 0.0174532925>rad Spherical GSE C2 Predicted Lat (GSE) E13.6 -90.0 90.0 LinearScale -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Scalar Positional Predicted Spacecraft 2, Cluster-Salsa, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic Spherical Coordinates Time Series defined by using: EPOCH__CL_JP_PGP sc_at2_long__CL_JP_PGP Predicted Spacecraft 2, Cluster-Salsa, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates, Angle from the X-axis in the GSE X-Y Plane Average Type: angle_degrees PT5M ° 0.0174532925>rad Spherical GSE C2 Predicted Long (GSE) E13.6 0.0 360.0 LinearScale 0.0 360.0 -1.0e+31 DirectionAngle.AzimuthAngle Scalar Positional Predicted Spacecraft 3, Cluster-Samba, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic Spherical Coordinates Time Series defined by using: EPOCH__CL_JP_PGP sc_at3_lat__CL_JP_PGP Predicted Spacecraft 3, Cluster-Samba, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates Average Type: angle_degrees PT5M ° 0.0174532925>rad Spherical GSE C3 Predicted Lat (GSE) E13.6 -90.0 90.0 LinearScale -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Scalar Positional Predicted Spacecraft 3, Cluster-Samba, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic Spherical Coordinates Time Series defined by using: EPOCH__CL_JP_PGP sc_at3_long__CL_JP_PGP Predicted Spacecraft 3, Cluster-Samba, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates, Angle from the X-axis in the GSE X-Y Plane Average Type: angle_degrees PT5M ° 0.0174532925>rad Spherical GSE C3 Predicted Long (GSE) E13.6 0.0 360.0 LinearScale 0.0 360.0 -1.0e+31 DirectionAngle.AzimuthAngle Scalar Positional Predicted Spacecraft 4, Cluster-Tango, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic Spherical Coordinates Time Series defined by using: EPOCH__CL_JP_PGP sc_at4_lat__CL_JP_PGP Predicted Spacecraft 4, Cluster-Tango, Spin Axis Attitude Latitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates Average Type: angle_degrees PT5M ° 0.0174532925>rad Spherical GSE C4 Predicted Lat (GSE) E13.6 -90.0 90.0 LinearScale -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Scalar Positional Predicted Spacecraft 4, Cluster-Tango, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic Spherical Coordinates Time Series defined by using: EPOCH__CL_JP_PGP sc_at4_long__CL_JP_PGP Predicted Spacecraft 4, Cluster-Tango, Spin Axis Attitude Longitude Angle, Geocentric Solar Ecliptic, GSE, Spherical Coordinates, Angle from the X-axis in the GSE X-Y Plane Average Type: angle_degrees PT5M ° 0.0174532925>rad Spherical GSE C4 Predicted Long (GSE) E13.6 0.0 360.0 LinearScale 0.0 360.0 -1.0e+31 DirectionAngle.AzimuthAngle Scalar Positional Predicted Spacecraft Tetrahedron Shape Quality Parameter G Time Series defined by using: EPOCH__CL_JP_PGP sc_config_QG__CL_JP_PGP Predicted Spacecraft Tetrahedron Shape Quality Parameter G, G=(Tetrahedron Volume/Ideal Volume)+(Tetrahedron Surface/Ideal Surface)+1 Average Type: standard PT5M 1>(G_qual) Q_G E13.6 1.0 3.0 LinearScale 1.0 3.0 -1.0e+31 Scalar Other Predicted Spacecraft Tetrahedron Shape Quality Parameter, R Time Series defined by using: EPOCH__CL_JP_PGP sc_config_QR__CL_JP_PGP Predicted Spacecraft Tetrahedron Shape Quality Parameter, R, R=norm*(Tetrahedron Volume/Sphere Volume)^1/3 Average Type: standard PT5M 1>(R_qual) Q_R E13.6 0.0 1.0 LinearScale 0.0 1.0 -1.0e+31 Scalar Other Predicted Spacecraft Separation Minimum Distance Time Series defined by using: EPOCH__CL_JP_PGP sc_dr_min__CL_JP_PGP Predicted Spacecraft Separation Minimum Distance Average Type: standard PT5M km 1.0e3>m Predicted Sep Min E13.6 0.0 20000.0 LogScale 0.0 1.0e+07 -1.0e+31 Magnitude Scalar Positional Predicted Spacecraft Separation Maximum Distance Time Series defined by using: EPOCH__CL_JP_PGP sc_dr_max__CL_JP_PGP Predicted Spacecraft Separation Maximum Distance Average Type: standard PT5M km 1.0e3>m Predicted Sep Max E13.6 1.0 20000.0 LogScale 0.0 1.0e+07 -1.0e+31 Magnitude Scalar Positional Predicted Coordinate System Rotation Angle, Geocentric Solar Ecliptic to Geocentric Solar Magnetospheric Time Series defined by using: EPOCH__CL_JP_PGP gse_gsm__CL_JP_PGP Predicted Coordinate System Rotation Angle, Geocentric Solar Ecliptic, GSE, to Geocentric Solar Magnetospheric, GSM Average Type: angle_degrees PT5M ° 0.0174532925>rad Spherical GSE Predicted GSE GSM E13.6 -90.0 90.0 LinearScale -40.0 40.0 -1.0e+31 DirectionAngle.AzimuthAngle Scalar Positional Predicted Magnetic Dipole Tilt Angle in the Geocentric Solar Magnetosphreric X-Z Plane Time Series defined by using: EPOCH__CL_JP_PGP dipole_tilt__CL_JP_PGP Predicted Magnetic Dipole Tilt Angle in the Geocentric Solar Magnetosphreric, GSM, X-Z Plane Average Type: angle_degrees PT5M ° 0.0174532925>rad Spherical GSM Predicted Pole Tilt E13.6 -90.0 90.0 LinearScale -40.0 40.0 -1.0e+31 DirectionAngle.AzimuthAngle Scalar Positional Predicted Spacecraft Tetrahedron Size Parameter, L Time Series defined by using: EPOCH__CL_JP_PGP sc_geom_size__CL_JP_PGP Predicted Spacecraft Tetrahedron Size Parameter, L, Characteristic Size Average Type: standard PT5M km 1.0e3>m Predicted Tetra L E13.6 1.0 100000.0 LogScale 0.0 1.0e+07 -1.0e+31 Scalar Other Predicted Spacecraft Tetrahedron Elongation Parameter, E Time Series defined by using: EPOCH__CL_JP_PGP sc_geom_elong__CL_JP_PGP Predicted Spacecraft Tetrahedron Elongation Parameter, E Average Type: standard PT5M 1>(Elongation) Predicted Tetra E E13.6 0.0 1.0 LinearScale 0.0 1.0 -1.0e+31 Scalar Other Predicted Spacecraft Tetrahedron Planarity Parameter, P Time Series defined by using: EPOCH__CL_JP_PGP sc_geom_planarity__CL_JP_PGP Predicted Spacecraft Tetrahedron Planarity Parameter, P Average Type: standard PT5M 1>(Planarity) Predicted Tetra P E13.6 0.0 1.0 LinearScale 0.0 1.0 -1.0e+31 Scalar Other Predicted Spacecraft Tetrahedron Elongation Direction Time Series defined by using: EPOCH__CL_JP_PGP sc_geom_E_dir_gse__CL_JP_PGP Predicted Spacecraft Tetrahedron Elongation Direction, expressed as Direction Cosines Average Type: standard PT5M 1.0>(direction) Spherical GSE E13.6 -1.0 1.0 LinearScale 3 Dir_elongation_x (GSE) 1 x (GSE) Dir_elongation_y (GSE) 2 y (GSE) Dir_elongation_z (GSE) 3 z (GSE) -1.0 1.0 -1.0e+31 Vector Positional Predicted Spacecraft Tetrahedron Planarity Normal Direction Time Series defined by using: EPOCH__CL_JP_PGP sc_geom_P_nor_gse__CL_JP_PGP Predicted Spacecraft Tetrahedron Planarity Normal Direction, expressed as Direction Cosines Average Type: standard PT5M 1.0>(direction) Spherical GSE E13.6 -1.0 1.0 LinearScale 3 Nor_planarity_x (GSE) 1 x (GSE) Nor_planarity_y (GSE) 2 y (GSE) Nor_planarity_z (GSE) 3 z (GSE) -1.0 1.0 -1.0e+31 Vector Positional