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/01/0113/02/00320/ 221198/140000001/ +022059.958/+001931.592/+060630.561/ +1.46776510/+2.04522088/+1.45994280/ ZZ INT/ITZ/01/0114/02/00324/ 081298/030000001/ +055746.798/+059765.769/+077964.149/ +0.77725566/+1.60206226/+0.07962691/ ZZ INT/ITZ/01/0115/02/00326/ 151298/120000001/ +038717.753/+028399.543/+071781.239/ +1.12974799/+1.91678296/+0.63048346/ ZZ INT/ITZ/01/0116/02/00328/ 231298/120000001/ +067617.787/+085806.504/+075349.990/ +0.54480752/+1.33417319/-0.21989616/ ZZ INT/ITZ/01/0117/02/00329/ 261298/200000001/ +034845.911/+020791.065/+068379.536/ +1.23048606/+1.99186435/+0.81456206/ ZZ