2.3.0 spase://ESA/NumericalData/Equator-S/Ephemeris/PrimeParameter/PT4S Equator-S Epheneris and Auxiliary Prime Parameter 4 s Data 2021-04-27T17:52:14Z Equator-S Auxiliary Data Prime Parameters. EQUATOR-S was a Low-Cost Mission designed to study the Earth's Equatorial Magnetosphere out to Distances of about 10 Re and it formed Element of the Closely-Coordinated Fleet of Satellites that comprise the IASTP Program. Equator-S was based on a Simple Spacecraft Design and carries a Science Payload consisting of advanced Instruments that were developed for other IASTP Missions. Unique Features of EQUATOR-S were its nearly Equatorial Orbit and its High Spin Rate. It was launched as an Auxiliary Payload on an Ariane-4 Rocket on December 2, 1997. The Mission was intended for a Two-Year Lifetime. See the Equator-S Data Center Manual, EQS-MPE-EDC-01, Section 4.8 AUX G. Paschmann, Refer to ESDS for Rules of Acknowledgement Refer to EQS-MPE-EDC-01. spase://SMWG/Person/Goetz.Paschmann PrincipalInvestigator spase://SMWG/Person/Robert.E.McGuire MetadataContact spase://SMWG/Person/Lee.Frost.Bargatze MetadataContact spase://VSPO/NumericalData/Equator-S/Ephemeris/PrimeParameter/PT4S spase://SMWG/Repository/NASA/GSFC/SPDF Online Open FTPS from SPDF (not with most browsers) ftps://spdf.gsfc.nasa.gov/pub/data//equator-s/pp/aux/ Access to Data in CDF Format via ftp from SPDF HTTPS from SPDF https://spdf.gsfc.nasa.gov/pub/data//equator-s/pp/aux/ Access to Data in CDF Format via http from SPDF CDAWeb https://cdaweb.gsfc.nasa.gov/cgi-bin/eval2.cgi?dataset=EQ_PP_AUX&index=sp_phys EQ_PP_AUX Access to ASCII, CDF, and plots via NASA/GSFC CDAWeb CDF None G. Paschmann, Refer to ESDS for Rules of Acknowledgement Refer to EQS-MPE-EDC-01. 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 EQ_PP_AUX Web Service to this product using the HAPI interface. CSV G. Paschmann, Refer to ESDS for Rules of Acknowledgement Refer to EQS-MPE-EDC-01. Please acknowledge the data providers and CDAWeb when using these data. Calibrated spase://SMWG/Instrument/Equator-S/Ephemeris Ephemeris 1997-12-16T11:25:00 1998-04-30T01:52:44 PT4S Earth.Magnetosphere Earth.Magnetosphere.Main Earth.Magnetosphere.RadiationBelt Earth.NearSurface.EquatorialRegion See also the TEXT Global Attribute for the Caveats File Location Epoch Time, since 0 A.D. Epoch Epoch Time, Milliseconds since 0 A.D., Interval Centered, rounded to nearest Millisecond This parameter exhibits an increasing monotonic progression. PT4S ms 1e-3>s Epoch 6.2924580219904e+13 6.3745034619904e+13 LinearScale 01-Jan-1994 00:00:00.000 01-Jan-2020 00:00:00.000 -1.0e+31 Temporal Spacecraft Status Time series defined by using: EPOCH sc_status Spacecraft Status, Scalar Average Type: none PT4S I3 0 255 2 Element 1 1 Element 2 2 0 255 255 InstrumentMode Spacecraft Position, GSE Time series defined by using: EPOCH sc_r_xyz_gse Spacecraft Position, Geocentric Solar Ecliptic, GSE, Cartesian Coordinates Average Type: standard PT4S km 1e3>m Cartesian GSE E13.6 -130000.0 130000.0 LinearScale 3 Element 1 1 x, GSE Element 2 2 y, GSE Element 3 3 z, GSE -150000.0 150000.0 -1.0e+31 Vector Positional Spacecraft Velocity, GSE Time series defined by using: EPOCH sc_v_xyz_gse Spacecraft Velocity, Geocentric Solar Ecliptic, GSE, Cartesian Coordinates Average Type: standard PT4S km/s 1e3>m/s Cartesian GSE E13.6 -10.0 10.0 LinearScale 3 Element 1 1 x, GSE Element 2 2 y, GSE Element 3 3 z, GSE -10.0 10.0 -1.0e+31 Vector Positional Spacecraft Latitude, GSE Time series defined by using: EPOCH sc_at_lat Spacecraft Latitude, Geocentric Solar Ecliptic, GSE, Spherical Coordinates Average Type: angle_degrees PT4S ° 0.0174532925>rad Spherical GSE Lat, GSE E13.6 -90.0 90.0 LinearScale -90.0 90.0 -1.0e+31 DirectionAngle.ElevationAngle Positional Spacecraft Longitude, GSE Time series defined by using: EPOCH sc_at_long Spacecraft Longitude, Geocentric Solar Ecliptic, GSE, Spherical Coordinates Average Type: angle_degrees PT4S ° 0.0174532925>rad Spherical GSE Long, GSE E13.6 0.0 360.0 LinearScale 0.0 360.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Telemetry Rate Time series defined by using: EPOCH tm_rate Telemetry Rate, Low or High, Scalar Average Type: none PT4S TM Rate E13.6 0.0 1.1 LinearScale 0.0 1.1 -1.0e-31 Other Rotation Angle, GSE to GSM Time series defined by using: EPOCH gse_gsm Rotation Angle, GSE to GSM, Scalar Average Type: angle_degrees PT4S ° 0.0174532925>rad Spherical GSE GSE_GSM E13.6 -35.0 35.0 LinearScale -35.0 35.0 -1.0e+31 DirectionAngle.AzimuthAngle Positional Dipole Tilt in the GSM X-Z Plane Time series defined by using: EPOCH dipole_tilt Dipole Tilt in the GSM X-Z Plane, Scalar Average Type: angle_degrees PT4S ° 0.0174532925>rad Spherical GSE Pole_Tilt E13.6 -35.0 35.0 LinearScale -35.0 35.0 -1.0e+31 DirectionAngle.ElevationAngle Positional