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/01/0038/01/00086/ 180696/100000000/ 84652.51520/106534.1403/120558.7267/ .1774534064/.6661903271/-.174435216/ 5881/ZZ INT/ITZ/01/0039/01/00088/ 260696/100000000/ 87682.45079/125690.9562/109538.0416/ -.013119494/.4129558603/-.430168274/ 5881/ZZ INT/ITZ/01/0043/01/00095/ 230796/120000000/ 81498.03813/136636.8604/82648.63699/ -.257966192/.0622685958/-.706524192/ 5884/ZZ 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