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/01/0119/02/00341/                                                       
100299/060000001/                                                               
+024884.738/+004562.449/+057421.729/                                            
+1.54037599/+2.14273036/+1.36360158/                                            
ZZ                                                                              
INT/ITZ/01/0120/02/00346/                                                       
020399/190000000/                                                               
+082665.665/+156414.081/+022938.170/                                            
-0.15888166/+0.26635673/-0.70160295/                                            
ZZ                                                                              
INT/ITZ/01/0121/02/00351/                                                       
220399/150000001/                                                               
+056587.280/+144686.101/-030523.127/                                            
-0.55822954/-0.63698829/-0.66204449/                                            
ZZ