2.2.6 spase://CDPP/NumericalData/AMDA/STEREO-A/Ephemeris/sta-l2-orb orbit STEREO-A orbit 2015-10-14T11:46:29Z STEREO-A orbit is calculated using SPICE kernels from https://sohowww.nascom.nasa.gov at IRAP spase://CDPP/Person/Elena.Budnik TechnicalContact spase://SMWG/Repository/CDPP/AMDA Online Open http://amda.cdpp.eu Text https://sohowww.nascom.nasa.gov spase://CDPP/Instrument/AMDA/STEREO-A/Ephemeris Ephemeris 2006-10-27T00:00:00Z 2018-11-29T00:00:00Z PT900S xyz_gse sta_gse pos.earth;instr.obsty Re Cartesian GSE TimeSeries 3 x 1 sta_gse(0) y 2 sta_gse(1) z 3 sta_gse(2) Positional distance sta-earth sta_r_gse pos.distance Re TimeSeries Positional xyz_hee sta_hee pos.heliocentric;pos.distance;instr.obsty AU Cartesian HEE TimeSeries 3 x 1 sta_hee(0) y 2 sta_hee(1) z 3 sta_hee(2) Positional distance sta-sun sta_r_hee pos.distance AU TimeSeries Positional