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/01/0017/01/00038/ 201295/150000000/ 66193.97311/125081.0443/68021.87314/ -.493877253/-.426545715/-.879715685/ 5862/ZZ INT/ITZ/01/0018/01/00040/ 271295/170000000/ 81505.68772/133465.6068/99764.10893/ -.248422974/.0219077733/-.596556783/ 5892/ZZ INT/ITZ/01/0019/01/00043/ 080196/140000000/ +065792.136/+126683.313/+067496.562/ -0.49402542/-0.39958710/-0.87530848/ 5896/ZZ INT/ITZ/01/0020/01/00045/ 160196/130000000/ 46546.43242/106303.7923/35737.58456/ -.754634708/-.941533626/-1.10910838/ 5879/ZZ INT/ITZ/01/0021/01/00046/ 190196/150000000/ 77911.68182/133770.4958/89963.00287/ -.318888871/-.075227779/-.683922510/ 5859/ZZ INT/ITZ/01/0022/01/00048/ 270196/150000000/ 62787.03889/124161.5347/60922.06156/ -.539719095/-.478541648/-.921501492/ 5882/ZZZ