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Post Info TOPIC: CZ-4B F-04 Debri Re-entry


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CZ-4B F-04 Debri Re-entry
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Debri from a Chinese CZ-4B F-04 Rocket Body that was launched on the 14th October, 1999, from the Taiyuan Satellite Launch Centre for the "ZiYuan" ZY-1(CBERS-1)/SACI-1 mission is predicted to re-enter the Earths atmosphere on the 9th June, 2010 @ --:-- GMT  ± -- hours.

TLE Data
CZ-4 DEB
1 26267U 99057FD 10159.56094052 .01625410 14754-2 38763-2 0 6011
2 26267 098.3795 182.6005 0010268 212.1145 147.9509 15.96872218556450

Period:                     90.36 minutes
Inclination:               98.38°
Apogee:                   299 km
Perigee:                   286 km
Revolution Number:    -
Size:                        0.09 metres
Predicted  Location:    -

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