DELTA 2 DEB
Satellite information DELTA 2 DEB
| Spacetrack Directory Name | DELTA 2 DEB |
| Orbit launches |
2006-09-25 |
| Deorbitation |
|
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| WWW | Here |
| Perigee | 239 km |
| Apogee | 10734 km |
| Height DELTA 2 DEB | 5654.03 km |
Additional information DELTA 2 DEB
DELTA 2 DEB, 38674 is space debris originally from a launch on Mon, 25 Sep 2006 UTC launched from the Air Force Eastern Test Range (AFETR). Debris objects in space refer to the collection of defunct objects orbiting the Earth. Examples of debris include non-operational satellites, rocket bodies, and fragments generated from explosions, collisions, or faulty payload assembly.
satellite DELTA 2 DEB Date of exalting 25.09.2006y. Average height of ISS DELTA 2 DEB hundred 5654.03 km. Average velocity DELTA 2 DEB is 20643.13 km/h. Inclination DELTA 2 DEB satellite 39.91°.Average velocity DELTA 2 DEB
Average inclination DELTA 2 DEB
Mean right ascension of the ascending node (RAAN) DELTA 2 DEB
Mean argument of perigee DELTA 2 DEB
Mean semi-major axis of the orbit DELTA 2 DEB
Mean orbital eccentricity DELTA 2 DEB
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