* Astronomy

A H-IIA Launch Vehicle No. 7, Stage 3 Rocket Body that was launched in February 2005 from the Tanegashima launch complex for the Multi-functional Transport Satellite-1 Replacement (MTSAT-1R) mission is predicted to re-enter the Earths atmosphere on the 18th July 2008 @ 14:59 UTC ± 18 hours

TLE Data

H-2 RB
1 28623U 05006B   08197.82369515  .13778788 -64223-5  48996-3 0  9065
2 28623 028.4896 076.6678 0697423 188.3780 170.4526 14.88250876 58946
1 28623U 05006B   08197.75660971  .13772465 -63882-5  48631-3 0  9058
2 28623 028.4924 077.1034 0705517 187.6688 171.2640 14.86400242 58930
1 28623U 05006B   08197.62271484  .13746282 -63236-5  50058-3 0  9047
2 28623 028.4932 077.9519 0720467 186.2833 175.6652 14.82693050 58919
1 28623U 05006B   08197.08132340  .12267651 -59896-5  29172-3 0  9030
2 28623 028.4940 081.3864 0799530 180.5533 180.5312 14.67165169 58838
1 28623U 05006B   08196.67169419  .11728083 -57793-5  50143-3 0  9026
2 28623 028.4847 083.8982 0827285 176.6969 183.9255 14.56663442 58771

Predicted Decay Location    21.8° S, 151.7° W
Inclination    28.4°
Revolution Number    5929