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/01/0047/01/00102/ 200896/100000000/ -3629.04914/18702.33276/-25463.0768/ -1.38335955/-4.37044184/.4177514607/ 5870/ZZ INT/ITZ/01/0048/01/00104/ 270896/100000000/ 50172.65461/116062.6240/22649.57362/ -.723626437/-.829615854/-1.05726040/ 5883/ZZ INT/ITZ/01/0049/01/00107/ 070996/160000000/ 58273.27686/124520.3552/33569.46103/ -.620555534/-.600618005/-1.00546718/ 5883/ZZ INT/ITZ/01/0050/01/00109/ 120996/140000000/ 29661.91478/-1009.95056/74998.98433/ 1.162263635/1.377899372/1.660562364/ 5868/ZZ INT/ITZ/01/0051/01/00114/ 011096/100000000/ 10925.24012/-18144.1035/47040.73544/ 1.509392946/1.162617261/2.817704488/ 5846/ZZ