2.3.2 spase://NASA/NumericalData/Wind/Ephemeris/predicted/PT10M Wind predicted Spacecraft Positions, 10 min Data https://doi.org/10.48322/73de-sf52 2021-05-31T12:34:56.789 2021-05-31T12:34:56.789 Updated to SPASE Version 2.3.2 if needed, Applied quality control for DOI usage, LFB Predicted (calculated) Wind spacecraft positions in various coordinate systems Wind Flight Operations Team (FOT); & Candey, Robert M. 2021-01-01T00:00:00 NASA Space Physics Data Facility spase://SMWG/Person/Robert.M.Candey DataProducer spase://SMWG/Person/Adam.Szabo Scientist spase://VHO/NumericalData/Wind/Ephemeris/predicted_PT10M spase://VSPO/NumericalData/Wind/Ephemeris/PT600S spase://VSPO/NumericalData/Wind/Ephemeris/predicted/PT10M spase://SMWG/Repository/NASA/GSFC/Wind Online Open Wind Spacecraft homepage https://wind.nasa.gov/ephemeris/pre/ Homepage for the Wind mission. Contains links to data and instrument descriptions. CDF None spase://SMWG/Repository/NASA/GSFC/SPDF Online Open FTPS from SPDF (not with most browsers) ftps://spdf.gsfc.nasa.gov/pub/data/wind/orbit/pre_or/ HTTPS from SPDF https://spdf.gsfc.nasa.gov/pub/data/wind/orbit/pre_or/ In CDF via HTTP from CDAWeb CDAWeb https://cdaweb.gsfc.nasa.gov/cgi-bin/eval2.cgi?dataset=WI_OR_PRE&index=sp_phys WI_OR_PRE CDF spase://SMWG/Repository/NASA/GSFC/SPDF Online Open CDAWeb HAPI Server https://cdaweb.gsfc.nasa.gov/hapi WI_OR_PRE Web Service to this product using the HAPI interface. CSV spase://SMWG/Instrument/Wind/Ephemeris Ephemeris 1997-04-06T00:00:00Z P0D PT10M Epoch Epoch Number of milliseconds since the epoch ms 1e-3>s -1.0e31 Temporal PB5 Time Time_PB5 PB5 Time value of point 3 Year 1 Day of year 2 Milisecond of day 3 -2147483648 Temporal GEI Position GCI_POS Position in Geocentric Equatorial Inertial coordinates (GEI, formerly GCI) km 1000>m Cartesian GEI 3 X Component.I 1 Y Component.J 2 Z Component.K 3 -1.8e+06 1.8e+06 -1.0e+31 Positional GEI Velocity GCI_VEL Spacecraft velocity in Geocentric Equatorial Inertial coordinates (GEI, formerly GCI) km/s 1000>m/s Cartesian GEI 3 Vx Component.I 1 Vy Component.J 2 Vz Component.K 3 -12.0 12.0 -1.0e+31 Other GSE Position GSE_POS Position in GSE coordinates km 1000>m Cartesian GSE 3 X Component.I 1 Y Component.J 2 Z Component.K 3 -1.8e+06 1.8e+06 -1.0e+31 Positional GSE Velocity GSE_VEL Velocity in GSE coordinates km/s 1000>m/s Cartesian GSE 3 Vx Component.I 1 Vy Component.J 2 Vz Component.K 3 -12.0 12.0 -1.0e+31 Other GSM Position GSM_POS Position in GSM coordinates km 1000>m Cartesian GSM 3 X Component.I 1 Y Component.J 2 Z Component.K 3 -1.8e+06 1.8e+06 -1.0e+31 Positional GSM Velocity GSM_VEL Velocity in GSM coordinates km/s 1000>m/s Cartesian GSM 3 Vx Component.I 1 Vy Component.J 2 Vz Component.K 3 -12.0 12.0 -1.0e+31 Other Sun Vector SUN_VECTOR Sun position vector in GEI (GCI) coordinates km 1000>m Cartesian GEI 3 X Component.I 1 Y Component.J 2 Z Component.K 3 -1.6e+08 1.6e+08 -1.0e+31 Positional HEC Position HEC_POS Position in HEC (SE) coordinates km 1000>m Cartesian SE 3 X Component.I 1 Y Component.J 2 Z Component.K 3 -1.8e+06 1.8e+06 -1.0e+31 Positional HEC Velocity HEC_VEL Velocity in HEC (SE) coordinates km/s 1000>m/s Cartesian SE 3 Vx Component.I 1 Vy Component.J 2 Vz Component.K 3 -12.0 12.0 -1.0e+31 Other Carrington Rotation Number CRN_EARTH Carrington rotation number: A method of numbering rotations of the sun based on a mean rotation period of sunspots of 27.2753 days, and starting with rotation number 1 on November 9, 1853. unitless 1857 2239 -2147483648 Other Heliographic Longitude of Earth LONG_EARTH Heliographic longitude of Earth rad Spherical HG 0.0 6.28319 -1.0e+31 DirectionAngle.AzimuthAngle Positional Heliographic Latitude of Earth LAT_EARTH Heliographic latitude of Earth rad Spherical HG -1.5708 1.5708 -1.0e+31 DirectionAngle.ElevationAngle Positional Heliographic Longitude of Spacecraft LONG_SPACE Heliographic longitude of the spacecraft rad Spherical HG 0.0 6.28319 -1.0e+31 DirectionAngle.AzimuthAngle Positional Heliographic Latitude of Spacecraft LAT_SPACE Heliographic latitude of the spacecraft rad Spherical HG -1.5708 1.5708 -1.0e+31 DirectionAngle.ElevationAngle Positional