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:           
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AAA                                                                             
INT/ITZ/01/0127/02/00395/                                                       
060999/090000001/                                                               
+005529.109/+060587.342/-055527.956/                                            
-0.92806836/-2.19878126/+0.32035470/                                            
ZZ                                                                              
INT/ITZ/01/0128/02/00405/                                                       
131099/090000001/                                                               
+062848.680/+155040.025/-032475.423/                                            
-0.47459518/-0.52919699/-0.54031213/                                            
ZZ