2.3.2 spase://NASA/NumericalData/Wind/Ephemeris/definitive/PT10M Wind Definitive Orbit, 10 min Data, Spacecraft Position and Velocity in GCI, GSE, GSM, HEC, and HG Coordinates https://doi.org/10.48322/t0jm-c908 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 Wind Definitive Orbit, Spacecraft Position and Velocity in Geocentric Celestial Inertial, GCI, Geocentric Solar Ecliptic, GSE, Geocentric Solar Magnetospheric, GSM, Heliospheric Ecliptic, HEC, and Heliographic, HG, Coordinates 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://SMWG/Person/Robert.E.McGuire MetadataContact spase://SMWG/Person/Lee.Frost.Bargatze MetadataContact Wind Spacecraft homepage https://wind.nasa.gov Homepage for the Wind mission. Contains links to data and instrument descriptions. 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://VHO/NumericalData/Wind/Ephemeris/predicted_PT10M spase://VHO/NumericalData/Wind/Ephemeris/definitive_PT10M spase://VSPO/NumericalData/Wind/Ephemeris/Definitive/PT10M spase://VSPO/NumericalData/Wind/Ephemeris/definitive/PT10M spase://SMWG/Repository/NASA/GSFC/Wind Online Open Wind Spacecraft Home Page https://wind.nasa.gov/ephemeris/def/ Homepage for the Wind mission. Contains links to data and instrument information. 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/def_or/ Access to Data in CDF Format via ftp from SPDF HTTPS from SPDF https://spdf.gsfc.nasa.gov/pub/data/wind/orbit/def_or/ Access to Data in CDF Format via http from SPDF CDAWeb https://cdaweb.gsfc.nasa.gov/cgi-bin/eval2.cgi?dataset=WI_OR_DEF&index=sp_phys WI_OR_DEF Access to ASCII, CDF, and plots via NASA/GSFC CDAWeb CDF None 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 WI_OR_DEF Web Service to this product using the HAPI interface. CSV Please acknowledge the data providers and CDAWeb when using these data. spase://SMWG/Instrument/Wind/Ephemeris Ephemeris 1994-11-01T10:47:18Z 1997-07-01T23:50:00Z PT10M Heliosphere Heliosphere.NearEarth Heliosphere.Inner Epoch Time, Orbit Epoch Epoch Time, Orbit This parameter exhibits an increasing monotonic progression. PT10M ms 1e-3>s Epoch 6.2877146619904e+13 6.3776657018904e+13 01-Jul-1992 00:00:00.000 31-Dec-2020 23:59:59.000 -1.0e+31 Temporal Time PB5, Orbit Time series defined by using: EPOCH Time_PB5 Time in PB5 Format: Year, Day, Milliseconds PT10M 3 Year 1 year 1992 2020 year 1992 2020 Day of Year (Jan 1 = day 1) 2 d 183 366 day 183 366 elapsed ms of day 3 ms 0 86399000 msec 0 86399000 -2147483648 Temporal Spacecraft Position, GCI Time series defined by using: EPOCH GCI_POS Spacecraft Position, Geocentric Inertial, GCI, Coordinates PT10M km 1e3>m Cartesian GEI F17.5 -1.8e+06 1.8e+06 3 Element 1 1 x Element 2 2 y Element 3 3 z -1.8e+06 1.8e+06 -1.0e+31 Vector Positional Spacecraft Velocity, GCI Time series defined by using: EPOCH GCI_VEL Spacecraft Velocity, Geocentric Inertial, GCI, Coordinates PT10M km/s 1e3>m/s Cartesian GEI F12.7 -12.0 12.0 3 vx 1 x vy 2 y vz 3 z -12.0 12.0 -1.0e+31 Vector Velocity Spacecraft Position, GSE Time series defined by using: EPOCH GSE_POS Spacecraft Position, Geocentric Solar Ecliptic, GSE, Coordinates PT10M km 1e3>m Cartesian GSE F17.5 -1.8e+06 1.8e+06 3 Element 1 1 x Element 2 2 y Element 3 3 z -1.8e+06 1.8e+06 -1.0e+31 Vector Positional Spacecraft Velocity, GSE Time series defined by using: EPOCH GSE_VEL Spacecraft Velocity, Geocentric Solar Ecliptic, GSE, Coordinates PT10M km/s 1e3>m/s Cartesian GSE F12.7 -12.0 12.0 3 vx 1 x vy 2 y vz 3 z -12.0 12.0 -1.0e+31 Vector Velocity Spacecraft Position, GSM Time series defined by using: EPOCH GSM_POS Spacecraft Position, Geocentric Solar Magnetospheric, GSM, Coordinates PT10M km 1e3>m Cartesian GSM F17.5 -1.8e+06 1.8e+06 3 Element 1 1 x Element 2 2 y Element 3 3 z -1.8e+06 1.8e+06 -1.0e+31 Vector Positional Spacecraft Velocity, GSM Time series defined by using: EPOCH GSM_VEL Spacecraft Velocity, Geocentric Solar Magnetospheric, GSM, Coordinates PT10M km/s 1e3>m/s Cartesian GSM F12.7 -12.0 12.0 3 vx 1 x vy 2 y vz 3 z vz 3 z -12.0 12.0 -1.0e+31 Vector Velocity Sun Position, GCI Time series defined by using: EPOCH SUN_VECTOR Sun Position, Geocentric Inertial, GCI, Coordinates PT10M km 1e3>m Cartesian GEI F17.5 -1.6e+08 1.6e+08 3 Element 1 1 x Element 2 2 y Element 3 3 z -1.6e+08 1.6e+08 -1.0e+31 Vector Positional Spacecraft Position, HEC Time series defined by using: EPOCH HEC_POS Spacecraft Position, Heliospheric Ecliptic, HEC, Coordinates PT10M km 1e3>m Cartesian HEE F17.5 -1.6e+08 1.6e+08 3 Element 1 1 x Element 2 2 y Element 3 3 z -1.6e+08 1.6e+08 -1.0e+31 Vector Positional Spacecraft Velocity, HEC Time series defined by using: EPOCH HEC_VEL Spacecraft Velocity, Heliospheric Ecliptic, HEC, Coordinates PT10M km/s 1e3>m/s Cartesian HEE F12.7 -35.0 35.0 3 vx 1 x vy 2 x vy 2 y vz 3 z -35.0 35.0 -1.0e+31 Vector Velocity Carrington Rotation Number, Earth Time series defined by using: EPOCH CRN_EARTH Carrington Rotation Number, Earth PT10M Spherical Carrington CRN I4 1857 2239 1857 2239 -2147483648 DirectionAngle.AzimuthAngle Positional Earth Longitude, HG Time series defined by using: EPOCH LONG_EARTH Earth Longitude, Heliographic, HG, Coordinates PT10M rad Spherical HG Helio Long F7.3 0.0 6.28319 0.0 6.28319 -1.0e+31 DirectionAngle.AzimuthAngle Positional Earth Latitude, HG Time series defined by using: EPOCH LAT_EARTH Earth Latitude, Heliographic, HG, Coordinates PT10M rad Spherical HG Helio Lat F7.3 -1.5708 1.5708 -1.5708 1.5708 -1.0e+31 DirectionAngle.ElevationAngle Positional Carrington Rotation Number, Spacecraft Time series defined by using: EPOCH CRN_SPACE Carrington Rotation Number, Spacecraft PT10M Spherical Carrington CRN Space I4 1857 2239 1857 2239 -2147483648 DirectionAngle.AzimuthAngle Positional Spacecraft Longitude, HG Time series defined by using: EPOCH LONG_SPACE Earth Longitude, Heliographic, HG, Coordinates PT10M rad Spherical HG Helio Long F7.3 0.0 6.28319 0.0 6.28319 -1.0e+31 DirectionAngle.AzimuthAngle Positional Spacecraft Latitude, HG Time series defined by using: EPOCH LAT_SPACE Earth Latitude, Heliographic, HG, Coordinates PT10M rad Spherical HG Helio Lat F7.3 -1.5708 1.5708 -1.5708 1.5708 -1.0e+31 DirectionAngle.ElevationAngle Positional