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/01/0116/02/00328/                                                       
231298/120000001/                                                               
+067617.787/+085806.504/+075349.990/                                            
+0.54480752/+1.33417319/-0.21989616/                                            
ZZ                                                                              
INT/ITZ/01/0117/02/00329/                                                       
261298/200000001/                                                               
+034845.911/+020791.065/+068379.536/                                            
+1.23048606/+1.99186435/+0.81456206/                                            
ZZ                                                                              
INT/ITZ/01/0118/02/00334/                                                       
140199/200000001/                                                               
+038927.282/+027318.998/+069225.395/                                            
+1.16182607/+1.96023604/+0.64572591/                                            
ZZ