2.2.2 spase://VMO/NumericalData/Interball-Tail/Ephemeris/PT2M Interball Tail definitive orbital data 2013-03-18T00:00:00.000 Definitive Interball Tail satellite and subsatellite (Interball-1 and Magion-4) orbital data: Spacecraft position, velocity, and status flags. The Interball project, Russian Space Research Institute (IKI) and Dr. Prokhorenko spase://SMWG/Person/Victoria.I.Prokhorenko PrincipalInvestigator spase://SMWG/Person/Jan.Merka MetadataContact IKI Satellite Situation Center http://www.iki.rssi.ru/vprokhor This page maintains the Situation Analysis for the IKI International Space Missions and its coordination with the Inter-Agency multimission campaigns. Interball Tail Probe Situation Analysis http://www.iki.rssi.ru/vprokhor/tail.htm spase://SMWG/Repository/NASA/GSFC/SPDF Online Open FTP access to files at SPDF ftp://cdaweb.gsfc.nasa.gov/pub/data/interball/tail/orbit In CDF via FTP from CDAWeb HTTP access to files at SPDF http://spdf.gsfc.nasa.gov/pub/data/interball/tail/orbit In CDF via HTTP from CDAWeb CDF None spase://SMWG/Repository/NASA/GSFC/SPDF Online Open CDAWeb http://cdaweb.gsfc.nasa.gov/sp_phys/ IT_OR_DEF Interball Tail definitive orbital data with subset, plot, and list functionalities from CDAWeb. SSCWeb http://sscweb.gsfc.nasa.gov/cgi-bin/Locator.cgi interballtail Text None spase://SMWG/Instrument/Interball-1/Ephemeris spase://SMWG/Instrument/Magion-4/Ephemeris Ephemeris 1995-08-07T00:00:00Z 2000-10-16T13:55:00.00Z PT2M Heliosphere.NearEarth Earth.Magnetosheath Earth.Magnetosphere Earth.Magnetosphere.Main Earth.Magnetosphere.Polar The data cadence varies. Time Epoch Time (centered) in miliseconds since CDF epoch ms 1e-3>s 01-Jan-1994 00:00:00.000 31-Dec-2020 23:59:59.000 -1.0E31 Temporal I1 position in GSE SC_pos_GSE Interball-1 spacecraft position in GSE frame, 3 components in RE (6370km) Re 6.37e6>m Cartesian GSE F7.3 3 I1 X (GSE) Component.I 1 -30.0 30.0 -1.0E31 I1 Y (GSE) Component.J 2 -30.0 30.0 -1.0E31 I1 Z (GSE) Component.K 3 -30.0 30.0 -1.0E31 Vector Positional I1 S/C position in GSM SC_pos_GSM Interball-1 spacecraft position in GSM frame, 3 components in RE (6370km) Re 6.37e6>m Cartesian GSM F7.3 3 I1 X (GSM) Component.I 1 -30.0 30.0 -1.0E31 I1 Y (GSM) Component.J 2 -30.0 30.0 -1.0E31 I1 Z (GSM) Component.K 3 -30.0 30.0 -1.0E31 Vector Positional I1 S/C velocity in GSE SC_vel_GSE Interball-1 spacecraft velocity in km/s in GSE frame km/s 1e3>m/s Cartesian GSE F7.3 3 I1 Vx (GSE) Component.I 1 -10.0 10.0 -1.0E31 I1 Vy (GSE) Component.J 2 -10.0 10.0 -1.0E31 I1 Vz (GSE) Component.K 3 -10.0 10.0 -1.0E31 Vector Velocity SC/SS separation in GSE SC/SS_sep_GSE Satellite-subsatellite separation (Interball-1 - Magion-4) vector in GSE km 1e3>m Cartesian GSE F8.1 3 dx GSE Component.I 1 -100000.0 100000.0 -1.0E31 dy GSE Component.J 2 -100000.0 100000.0 -1.0E31 dz GSE Component.K 3 -100000.0 100000.0 -1.0E31 Vector Positional Flag_O SF_SC_orbit Status Flag, Orbit : 0-good data, 1-bad data, 2-missing data 0 5 128 Other Flag_S SF_SC_sep Status Flag, Separation: 0-good data, 1-bad data, 2-missing data 0 5 128 Other Gap Flag Gap_Flag Post Gap Flag: 0 no gap before this point, 1-5 gap reason 0 5 -2147483648 Other