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/01/0131/01/00422/                                                       
151299/090000001/                                                               
+080191.953/+133375.098/+035175.016/                                            
+0.26415836/+0.91265478/-0.46238956/                                            
5887/ZZ                                                                         
INT/ITZ/01/0132/01/00430/                                                       
170100/090000001/                                                               
-005748.851/+021300.405/-038204.465/                                            
-0.91326644/-3.25566132/+1.65759323/                                            
5846/ZZ