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/01/0129/01/00410/                                                       
021199/090000001/                                                               
-000255.637/+039583.211/-049587.493/                                            
-0.97218416/-2.65488924/+0.83162631/                                            
5894/ZZ