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/01/0138/01/00485/ 100800/090000001/ +085707.442/+147395.962/+011144.562/ +0.21508169/+0.77721309/-0.36896552/ 5881/ZZ INT/ITZ/01/0139/01/00492/ 060900/090000001/ +090652.555/+169552.111/-004827.213/ -0.00582109/+0.36385929/-0.36500143/ 5858/ZZ INT/ITZ/01/0140/01/00498/ 280900/090000001/ +078745.996/+124706.105/+016546.904/ +0.43819158/+1.09486417/-0.31758848/ 5908/ZZ INT/ITZ/01/0141/01/00501/ 101000/090000001/ +091624.274/+165184.054/-002006.280/ +0.06986337/+0.46040469/-0.34875199/ 5848/ZZ