NIMBUS 2 DEB
Satellite information NIMBUS 2 DEB - 0 NIMBUS 2 DEB
| Spacetrack Directory Name | NIMBUS 2 DEB |
| Alternative name | 0 NIMBUS 2 DEB |
| Follow NIMBUS 2 DEB | NIMBUS 2 DEB Tracker |
| Pass predictions NIMBUS 2 DEB | Pass predictions NIMBUS 2 DEB |
| Orbit launches |
1966-05-15 (60 years ago)
|
| Days in orbit | 22026 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 1016 km |
| Apogee | 1076 km |
| Orbit slope (inclination) | 100.61° |
| Laps per day | 14 |
| Height NIMBUS 2 DEB | 1058.02 km |
Additional information NIMBUS 2 DEB
NIMBUS 2 DEB, 59976 is space debris in SSO originally from a launch on Sun, 15 May 1966 UTC launched from the Air Force Western Test Range (AFWTR). 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 NIMBUS 2 DEB Date of exalting 15.05.1966y. Average height of ISS NIMBUS 2 DEB hundred 1058.02 km. Average velocity NIMBUS 2 DEB is 26368.27 km/h. Inclination NIMBUS 2 DEB satellite 100.61°.TLE
Average velocity NIMBUS 2 DEB
Average inclination NIMBUS 2 DEB
Mean right ascension of the ascending node (RAAN) NIMBUS 2 DEB
Mean argument of perigee NIMBUS 2 DEB
Mean semi-major axis of the orbit NIMBUS 2 DEB
Mean orbital eccentricity NIMBUS 2 DEB
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