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/01/0100/01/00251/
060398/123000001/
76829.56147/97255.89656/91094.18064/
.3422909244/1.041900058/-.314076887/
5848/ZZ
INT/ITZ/01/0101/02/00258/
010498/123000001/
+048361.818/+035970.946/+090206.901/
+0.87835374/+1.57356972/+0.46335331/
ZZ
INT/ITZ/01/0102/02/00260/
090498/123000001/
+071897.828/+085170.723/+093056.311/
+0.45361862/+1.16875998/-0.19655250/
ZZ
INT/ITZ/01/0103/01/00262/
160498/123000001/
33106.89919/11543.96293/79181.80502/
1.139417593/1.732380485/1.011728263/
5875/ZZ