USA 40 R/B DEB
Satellite information USA 40 R/B DEB
| Spacetrack Directory Name | USA 40 R/B DEB |
| Follow USA 40 R/B DEB | USA 40 R/B DEB Tracker |
| Pass predictions USA 40 R/B DEB | Pass predictions USA 40 R/B DEB |
| Orbit launches |
1989-08-08 (37 years ago)
|
| Days in orbit | 13545 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 461 km |
| Apogee | 5642 km |
| Orbit slope (inclination) | 56.9° |
| Laps per day | 10 |
| Height USA 40 R/B DEB | 2722.56 km |
Additional information USA 40 R/B DEB
USA 40 R/B DEB, 23381 is space debris in LEO originally from a launch on Tue, 08 Aug 1989 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 USA 40 R/B DEB Date of exalting 08.08.1989y. Average height of ISS USA 40 R/B DEB hundred 2722.56 km. Average velocity USA 40 R/B DEB is 23825.65 km/h. Inclination USA 40 R/B DEB satellite 56.9°.TLE
Average velocity USA 40 R/B DEB
Average inclination USA 40 R/B DEB
Mean right ascension of the ascending node (RAAN) USA 40 R/B DEB
Mean argument of perigee USA 40 R/B DEB
Mean semi-major axis of the orbit USA 40 R/B DEB
Mean orbital eccentricity USA 40 R/B DEB
ISS
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