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/01/0072/01/00151/ 190297/180000000/ 71561.36191/70957.42006/112942.0414/ .4589428568/1.080461984/.0905129657/ 5906/ZZ INT/ITZ/01/0073/01/00154/ 030397/100000000/ 80576.92878/95570.21005/111606.6040/ .2749785540/.8753672585/-.188979191/ 5875/ZZ INT/ITZ/01/0074/01/00158/ 190397/100000000/ 84203.54686/136865.8744/77332.24729/ -.159219987/.2654220476/-.702571034/ 5874/ZZ INT/ITZ/01/0075/01/00160/ 280397/100000000/ 11878.82332/58898.87163/-32992.5837/ -1.21970031/-2.42305071/-.624121367/ 5901/ZZ