USA 40 R/B
Satellite information USA 40 R/B
| Spacetrack Directory Name | USA 40 R/B |
| Follow USA 40 R/B | USA 40 R/B Tracker |
| Pass predictions USA 40 R/B | Pass predictions USA 40 R/B |
| 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) |
| WWW | Here |
| Perigee | 534 km |
| Apogee | 8061 km |
| Orbit slope (inclination) | 57.01° |
| Laps per day | 8 |
| Height USA 40 R/B | 4958.95 km |
Additional information USA 40 R/B
USA 40 R/B, 20344 is space debris 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 Date of exalting 08.08.1989y. Average height of ISS USA 40 R/B hundred 4958.95 km. Average velocity USA 40 R/B is 21308.05 km/h. Inclination USA 40 R/B satellite 57.01°.TLE
Average velocity USA 40 R/B
Average inclination USA 40 R/B
Mean right ascension of the ascending node (RAAN) USA 40 R/B
Mean argument of perigee USA 40 R/B
Mean semi-major axis of the orbit USA 40 R/B
Mean orbital eccentricity USA 40 R/B
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