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/01/0001/03/00001/ 030895/010415527/ -2972.47183/-5047.05834/-4162.80961/ 2.267547343/-7.52823005/6.726315946/ 5683/ZZ INT/ITZ/01/0002/01/00003/ 070895/060000000/ 50471.86784/34248.07060/86588.08177/ .8249224091/1.233387984/1.201856222/ 5873/ZZ INT/ITZ/01/0003/01/00003/ 090895/080000000/ 76248.18148/132011.1822/105784.9180/ -.307325295/-.079443176/-.563589007/ 5849/ZZ INT/ITZ/01/0004/01/00004/ 140895/030000000/ 26694.66561/79170.69391/27270.35461/ -.962533440/-1.54775474/-1.36804320/ 5888/ZZ 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