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/01/0028/01/00063/ 220396/140000000/ 75207.01070/74374.24368/122423.8265/ .4010896948/.8997422796/.2804587794/ 5846/ZZ INT/ITZ/01/0029/01/00065/ 010496/150000000/ 31513.41320/85477.17407/9387.679965/ -1.00184234/-1.52093000/-1.22851089/ 5872/ZZ INT/ITZ/01/0030/01/00068/ 100496/150000000/ 76272.29383/78036.96581/123412.9855/ .3816732863/.8757746316/.2172184147/ 5868/ZZ INT/ITZ/01/0031/01/00070/ 190496/090000000/ 86149.76284/131945.1538/102382.6464/ -.157078837/.1794666189/-.558472941/ 5879/ZZ INT/ITZ/01/0032/01/00072/ 270496/140000000/ 69710.30182/128990.4174/62949.38380/ -.464555997/-.337429208/-.887470566/ 5920/ZZ