2.4.1 spase://CNES/NumericalData/CDPP-AMDA/INTERBALL-Tail/Ephemeris/intt-orb-all orbit 2013-05-24T12:42:32Z 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 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/CDPP/AMDA Online Open CDPP/AMDA HAPI Server https://amda.irap.omp.eu/service/hapi intt-orb-all Web Service to this product using the HAPI interface. CSV Thank you for acknowledging the use of AMDA in publications with wording like "Data analysis was performed with the AMDA science analysis system provided by the Centre de Données de la Physique des Plasmas (CDPP) supported by CNRS, CNES, Observatoire de Paris and Université Paul Sabatier, Toulouse". See the Rules of the road at https://amda.cdpp.eu/help/policy.html . Please acknowledge the Data Providers. spase://SMWG/Repository/CDPP/AMDA Online Open CDPP/AMDA Web application https://amda.cdpp.eu Access to Data via CDPP/AMDA Web application. CSV VOTable CDF PNG Thank you for acknowledging the use of AMDA in publications with wording like "Data analysis was performed with the AMDA science analysis system provided by the Centre de Données de la Physique des Plasmas (CDPP) supported by CNRS, CNES, Observatoire de Paris and Université Paul Sabatier, Toulouse". See the Rules of the road at https://amda.cdpp.eu/help/policy.html . Please acknowledge the Data Providers. CDAWeb spase://CNES/Instrument/CDPP-AMDA/Interball-1/Ephemeris Ephemeris 1995-08-04T00:01:00Z 2000-10-16T13:55:00Z PT2M Earth.Magnetosphere Earth.Magnetosheath Earth.Magnetosphere.Main Heliosphere.NearEarth The data cadence varies xyz_gse it_xyz Interball-1 spacecraft position in GSE frame, 3 components in RE (6370km) pos.ephem;pos.earth;instr.obsty Re 6.37e6>m Cartesian GSE TimeSeries F7.3 3 x Component.I 1 it_xyz(0) -30.0 30.0 -1.0E31 y Component.J 2 it_xyz(1) -30.0 30.0 -1.0E31 z Component.K 3 it_xyz(2) -30.0 30.0 -1.0E31 Vector Positional xyz_gsm it_xyz_gsm Interball-1 spacecraft position in GSM frame, 3 components in RE (6370km) pos.ephem;pos.earth;instr.obsty Re 6.37e6>m Cartesian GSM TimeSeries F7.3 3 x Component.I 1 it_xyz_gsm(0) -30.0 30.0 -1.0E31 y Component.J 2 it_xyz_gsm(1) -30.0 30.0 -1.0E31 z Component.K 3 it_xyz_gsm(2) -30.0 30.0 -1.0E31 Vector Positional