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/01/0064/01/00136/ 241296/090000000/ 45761.99540/25857.46576/98397.51077/ .8488466666/1.360971297/.8312722984/ 5898/ZZ INT/ITZ/01/0065/01/00137/ 281296/020000000/ 39391.12759/14942.49631/91140.86216/ .9574410736/1.413342992/1.070830149/ 5892/ZZ INT/ITZ/01/0066/01/00139/ 050197/160000000/ 83518.43730/107831.7534/110158.0428/ .1884401509/.7405435973/-.292719546/ 5883/ZZ INT/ITZ/01/0067/01/00141/ 130197/190000000/ 85818.60161/133209.0105/88427.26622/ -.088132287/.3619031314/-.611767967/ 5722/ZZ INT/ITZ/01/0068/01/00143/ 200197/140000000/ 77379.76712/88172.62085/113592.2210/ .3391670850/.9369926052/-.087630380/ 5905/ZZ INT/ITZ/01/0069/01/00145/ 280197/210000000/ 86323.90122/129947.0270/92325.57779/ -.044399576/.4399206245/-.568401169/ 5892/ZZ INT/ITZ/01/0070/01/00147/ 030297/180000000/ 9443.427696/-21610.7939/46947.50616/ 1.515596772/1.169277746/2.761946308/ 5872/ZZ