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/01/0031/01/00070/ 190496/090000000/ 86149.76284/131945.1538/102382.6464/ -.157078837/.1794666189/-.558472941/ 5879/ZZ INT/ITZ/01/0032/01/00072/ 270496/140000000/ 69710.30182/128990.4174/62949.38380/ -.464555997/-.337429208/-.887470566/ 5920/ZZ INT/ITZ/01/0033/01/00075/ 070596/070000000/ 77548.25724/84435.77086/123981.5394/ .3487378079/.8398789689/.1220468609/ 5881/ZZ INT/ITZ/01/0034/01/00077/ 140596/100000000/ 57500.37503/44383.76804/108961.0205/ .6687126358/1.141447651/.6774828635/ 5896/ZZ 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