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/01/0080/01/00179/ 060697/100000000/ 80728.66597/105212.3635/103447.5178/ .2468798308/.8326788721/-.325346051/ 5874/ZZ INT/ITZ/01/0081/01/00184/ 260697/100000000/ 77612.57378/143405.9188/47064.01825/ -.310659983/-.017140383/-.849040940/ 5884/ZZ INT/ITZ/01/0082/01/00187/ 080797/100000000/ 51011.17091/123663.7254/-3286.04509/ -.694868465/-.819565877/-.961159036/ 5906/ZZ INT/ITZ/01/0083/01/00191/ 210797/120000000/ 65808.13707/63853.73552/105665.7882/ .5566782956/1.222449164/.1162211432/ 5843/ZZ