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/01/0050/01/00109/ 120996/140000000/ 29661.91478/-1009.95056/74998.98433/ 1.162263635/1.377899372/1.660562364/ 5868/ZZ INT/ITZ/01/0051/01/00114/ 011096/100000000/ 10925.24012/-18144.1035/47040.73544/ 1.509392946/1.162617261/2.817704488/ 5846/ZZ INT/ITZ/01/0052/01/00116/ 111096/100000000/ 76483.64318/136197.2923/64128.10577/ -.359585066/-.114789105/-.836688812/ 5851/ZZ INT/ITZ/01/0053/01/00119/ 231096/000000000/ 69550.50038/132865.3191/48255.25855/ -.469769699/-.324669843/-.924986630/ 5880/ZZ INT/ITZ/01/0054/01/00121/ 281096/130000000/ 56975.34464/44252.50705/109789.7177/ .6724354735/1.198469456/.5444781489/ 5888/ZZ