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/01/0083/01/00191/ 210797/120000000/ 65808.13707/63853.73552/105665.7882/ .5566782956/1.222449164/.1162211432/ 5843/ZZ INT/ITZ/01/0084/01/00195/ 050897/120000000/ 56463.98260/43630.60934/101531.5010/ .7186333606/1.370828299/.3870184035/ 5888/ZZ INT/ITZ/01/0085/01/00197/ 140897/120000000/ 82319.39558/142096.1138/60751.79577/ -.194544879/.2224613338/-.766778574/ 5883/ZZ 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