* Astronomy

Blobrana · L

RE: DNEPR 1 rocket body re-entry

Blobrana · L

Update:
A DNEPR 1 rocket body (debris) re-entered the Earths atmosphere on the 10th June, 2012 @ 12:40 GMT ± 50 minutes.

Inclination: 64.50°
Revolution Number: 64735
Predicted Location: 10.4°N, 257°E

Blobrana · L

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Blobrana · L

Update:
A DNEPR 1 rocket body (debris) is predicted to re-enter the Earths atmosphere on the 10th June, 2012 @ 14:30 GMT ± 14 hours.

DNEPR 1
1 26551U 00057G   12161.60276683  .04556808  75666-5  18186-2 0  8020
2 26551 064.5047 343.4257 0020137 267.3786 092.9232 16.22663336647199

Period:       89.5 minutes
Inclination: 64.50°
Apogee:     265 km
Perigee:     235 km
Revolution Number: 64735
Predicted Location:   57°N, 273.3°E

Blobrana · L

Update:
A DNEPR 1 rocket body (debris) is predicted to re-enter the Earths atmosphere on the 10th June, 2012 @ 12:15 GMT ± 24 hours.

DNEPR 1
1 26551U 00057G   12160.67594843  .03149046  74438-5  22073-2 0  7966
2 26551 064.5082 346.9478 0023961 273.7201 086.1797 16.15173023647048

Period:       89.5 minutes
Inclination: 64.51°
Apogee:     265 km
Perigee:     235 km
Revolution Number: 64733
Predicted Location:   63°S, 148.4°E

Blobrana · L

A DNEPR 1 rocket body (debris) that was launched on the 26th September, 2000, from the Baikonur Cosmodrome, for the MEGSAT 1, TIUNGSAT 1, UNISAT and SAUDISAT 1A &1B satellite missions is predicted to re-enter the Earths atmosphere on the 9th June, 2012 @ 07:00 GMT ± 72 hours.

DNEPR 1
1 26551U 00057G   12157.56596785  .01489236  13185-2  24852-2 0  7802
2 26551 064.5111 358.5885 0023844 264.7332 095.0792 16.02326178646542

Period:       89.35 minutes
Inclination: 64.51°
Apogee:     285 km
Perigee:     256 km
Revolution Number: 64715
Predicted Location:   22.3°N, 355.2°E