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/01/0035/01/00079/ 230596/100000000/ 87089.12858/130156.3644/105145.9223/ -.088542556/.2837704440/-.509085483/ 5894/ZZ INT/ITZ/01/0036/01/00081/ 310596/100000000/ 80956.26400/135351.7110/83061.03221/ -.273615251/-.013837780/-.721984029/ 5870/ZZ INT/ITZ/01/0037/01/00083/ 070696/030000000/ 86211.02703/112159.5425/119698.6691/ .1280601720/.5928970731/-.233797441/ 5887/ZZ 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