ATLAS 28E DEB
Satellite information ATLAS 28E DEB
| Spacetrack Directory Name | ATLAS 28E DEB |
| Follow ATLAS 28E DEB | ATLAS 28E DEB Tracker |
| Pass predictions ATLAS 28E DEB | Pass predictions ATLAS 28E DEB |
| Orbit launches |
1990-04-11 (36 years ago)
|
| Days in orbit | 13288 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 589 km |
| Apogee | 671 km |
| Orbit slope (inclination) | 89.85° |
| Laps per day | 15 |
| Height ATLAS 28E DEB | 614.76 km |
Additional information ATLAS 28E DEB
ATLAS 28E DEB, 20564 is space debris in LEO originally from a launch on Wed, 11 Apr 1990 UTC via an ATLAS E ALTAIR launch vehicle 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 ATLAS 28E DEB Date of exalting 11.04.1990y. Average height of ISS ATLAS 28E DEB hundred 614.76 km. Average velocity ATLAS 28E DEB is 27191.25 km/h. Inclination ATLAS 28E DEB satellite 89.85°.TLE
Average velocity ATLAS 28E DEB
Average inclination ATLAS 28E DEB
Mean right ascension of the ascending node (RAAN) ATLAS 28E DEB
Mean argument of perigee ATLAS 28E DEB
Mean semi-major axis of the orbit ATLAS 28E DEB
Mean orbital eccentricity ATLAS 28E DEB
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