COSMOS 886 DEB
Satellite information COSMOS 886 DEB
| Spacetrack Directory Name | COSMOS 886 DEB |
| Follow COSMOS 886 DEB | COSMOS 886 DEB Tracker |
| Pass predictions COSMOS 886 DEB | Pass predictions COSMOS 886 DEB |
| Orbit launches |
1976-12-27 (49 years ago)
|
| Days in orbit | 18185 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 570 km |
| Apogee | 1999 km |
| Orbit slope (inclination) | 65.8° |
| Laps per day | 13 |
| Height COSMOS 886 DEB | 1301.2 km |
Additional information COSMOS 886 DEB
COSMOS 886 DEB, 9823 is space debris in LEO originally from a launch on Mon, 27 Dec 1976 UTC launched from the Tyuratam Missile And Space Complex (TTMTR). 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 COSMOS 886 DEB Date of exalting 27.12.1976y. Average height of ISS COSMOS 886 DEB hundred 1301.2 km. Average velocity COSMOS 886 DEB is 25947.2 km/h. Inclination COSMOS 886 DEB satellite 65.8°.TLE
Average velocity COSMOS 886 DEB
Average inclination COSMOS 886 DEB
Mean right ascension of the ascending node (RAAN) COSMOS 886 DEB
Mean argument of perigee COSMOS 886 DEB
Mean semi-major axis of the orbit COSMOS 886 DEB
Mean orbital eccentricity COSMOS 886 DEB
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