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/01/0005/01/00006/ 210895/050000000/ 58776.14370/120342.7907/74131.71168/ -.542430729/-.511650387/-.880775068/ 5855/ZZ INT/ITZ/01/0006/01/00008/ 270895/170000000/ 86796.50085/125390.1105/125767.9922/ -.077030688/.2954578178/-.245238452/ 5869/ZZ INT/ITZ/01/0007/01/00010/ 040995/070000000/ 87066.02231/125260.5966/125713.1434/ -.070343960/.3000219259/-.244510568/ 5856/ZZ INT/ITZ/01/0008/01/00012/ 110995/100000000/ 86539.45162/107889.2465/130175.3593/ .1165671950/.5513756111/.0299434049/ 5855/ZZ INT/ITZ/01/0009/01/00015/ 230995/100000000/ 86370.81996/127987.5009/121325.4705/ -.124899418/.2183033663/-.341979340/ 5864/ZZ