Format: F1 Orbital data as a state vectors, index : 1 Project: INT Satellite: ITP Synonimus: ITZ Launch date: 19950803 ----- TAIL PROBE, INTERBALL PROJECT ----- PROJ.launch: 19950803 Inertial coordinate system corresponds to equinox of equator of epoc: J2000 Situation calculation index : 2 Orbit calculation index: 3120300 GPC file name: gemt2.17 Harm. level : 4 Planets perturbation: ------------------------------------------------------------------------------ AAA INT/ITZ/01/0132/01/00430/ 170100/090000001/ -005748.851/+021300.405/-038204.465/ -0.91326644/-3.25566132/+1.65759323/ 5846/ZZ INT/ITZ/01/0133/01/00440/ 220200/090000001/ +084380.380/+170484.761/-003139.295/ -0.14894721/+0.18133226/-0.50432421/ 5836/ZZ