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/01/0086/01/00199/ 230897/100000000/ 13486.32491/67132.66433/-39863.0740/ -1.11090072/-2.15617105/-.543924772/ 5889/ZZ INT/ITZ/01/0087/01/00200/ 260897/210000000/ 41320.88944/113351.5633/-17064.0291/ -.801670885/-1.08315131/-.921517938/ 5846/ZZ INT/ITZ/01/0088/01/00204/ 080997/210000000/ 68196.93392/68606.94709/105080.5740/ .5205493598/1.196006607/.0390036211/ 5907/ZZ INT/ITZ/01/0089/01/00208/ 260997/123000001/ 18615.25753/77077.12283/-38725.5708/ -1.05332366/-1.90520825/-.646305849/ 5898/ZZ