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/01/0021/01/00046/ 190196/150000000/ 77911.68182/133770.4958/89963.00287/ -.318888871/-.075227779/-.683922510/ 5859/ZZ INT/ITZ/01/0022/01/00048/ 270196/150000000/ 62787.03889/124161.5347/60922.06156/ -.539719095/-.478541648/-.921501492/ 5882/ZZZ INT/ITZ/01/0023/01/00050/ 040296/130000000/ 43408.28579/104210.9668/30947.00733/ -.792452361/-1.01204634/-1.13174871/ 5836/ZZ INT/ITZ/01/0024/01/00052/ 100296/160000000/ 88195.08397/121734.3586/120153.0841/ -.012560614/.4172498705/-.300273383/ 5852/ZZ INT/ITZ/01/0025/01/00054/ 190296/150000000/ 49183.32004/111346.4847/39058.73895/ -.718298213/-.829537562/-1.07440360/ 5869/ZZ