USA 142 DEB
Satellite information USA 142 DEB
| Spacetrack Directory Name | USA 142 DEB |
| Follow USA 142 DEB | USA 142 DEB Tracker |
| Pass predictions USA 142 DEB | Pass predictions USA 142 DEB |
| Orbit launches |
1999-04-09 (27 years ago)
|
| Days in orbit | 10013 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 616 km |
| Apogee | 35684 km |
| Orbit slope (inclination) | 28.74° |
| Laps per day | 2 |
| Height USA 142 DEB | 24385.62 km |
Additional information USA 142 DEB
USA 142 DEB, 44436 is space debris in HEO originally from a launch on Fri, 09 Apr 1999 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 142 DEB Date of exalting 09.04.1999y. Average height of ISS USA 142 DEB hundred 24385.62 km. Average velocity USA 142 DEB is 12420.47 km/h. Inclination USA 142 DEB satellite 28.77°.TLE
Average velocity USA 142 DEB
Average inclination USA 142 DEB
Mean right ascension of the ascending node (RAAN) USA 142 DEB
Mean argument of perigee USA 142 DEB
Mean semi-major axis of the orbit USA 142 DEB
Mean orbital eccentricity USA 142 DEB
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