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/01/0137/02/00477/ 100700/090000001/ +057851.189/+080662.155/+030962.783/ +0.83988310/+1.74772833/-0.16359141/ ZZ INT/ITZ/01/0138/02/00485/ 100800/090000001/ +085698.561/+147416.586/+010854.677/ +0.21483213/+0.77665880/-0.37060387/ ZZ INT/ITZ/01/0139/02/00492/ 060900/090000001/ +090641.032/+169541.966/-005110.008/ -0.00535272/+0.36294226/-0.36611996/ ZZ INT/ITZ/01/0140/02/00498/ 280900/090000001/ +078768.740/+124637.572/+016878.879/ +0.43782097/+1.09621791/-0.31391471/ ZZ