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/01/0135/01/00463/                                                       
200500/090000001/                                                               
+069321.925/+163393.695/-034640.726/                                            
-0.40169957/-0.48465123/-0.36188042/                                            
5879/ZZ                                                                         
INT/ITZ/01/0136/01/00470/                                                       
150600/090000001/                                                               
+083648.139/+175813.116/-016884.997/                                            
-0.18497178/-0.00797576/-0.40669140/                                            
5906/ZZ