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/01/0044/01/00096/ 250796/120000000/ 51988.49232/32321.67864/102087.1195/ .7685250193/1.252842390/.8108587238/ 5856/ZZ INT/ITZ/01/0045/01/00098/ 020896/070000000/ 63930.11163/52001.00230/112718.7047/ .5860889165/1.124748049/.4726774608/ 5890/ZZ INT/ITZ/01/0046/01/00101/ 130896/140000000/ 58449.75419/41173.05490/107804.2344/ .6762529055/1.198827983/.6253459137/ 5869/ZZ INT/ITZ/01/0047/01/00102/ 200896/100000000/ -3629.04914/18702.33276/-25463.0768/ -1.38335955/-4.37044184/.4177514607/ 5870/ZZ INT/ITZ/01/0048/01/00104/ 270896/100000000/ 50172.65461/116062.6240/22649.57362/ -.723626437/-.829615854/-1.05726040/ 5883/ZZ