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/01/0118/01/00334/                                                       
140199/200000001/                                                               
+038981.454/+027380.954/+069204.846/                                            
+1.15970041/+1.96116539/+0.64431678/                                            
5886/ZZ