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/01/0009/01/00015/ 230995/100000000/ 86370.81996/127987.5009/121325.4705/ -.124899418/.2183033663/-.341979340/ 5864/ZZ INT/ITZ/01/0010/01/00021/ 171095/060000000/ 55734.37015/114070.6515/60193.50969/ -.616992495/-.661546315/-.989032276/ 5863/ZZ INT/ITZ/01/0011/01/00024/ 271095/070000000/ 88374.67865/120245.3074/127005.9760/ .0185611205/.3897256378/-.199616452/ 5879/ZZZ INT/ITZ/01/0012/01/00026/ 021195/160000000/ 55314.69454/42049.21975/99773.70012/ .7172391120/1.136329687/.9343622750/ 5877/ZZ