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/01/0074/01/00158/ 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 INT/ITZ/01/0076/01/00163/ 070497/100000000/ 84080.25798/137644.4083/74554.44573/ -.168083899/.2332452349/-.724023460/ 5872/ZZ INT/ITZ/01/0077/01/00164/ 110497/100000000/ 80183.23334/140764.8553/60243.48127/ -.270556767/.0525512236/-.814677676/ 5868/ZZ INT/ITZ/01/0078/01/00168/ 250497/100000000/ 75827.84283/86650.42146/111399.1610/ .3712947535/.9734349677/-.111250684/ 5870/ZZ