COSMOS 252 DEB
Satellite information COSMOS 252 DEB
| Spacetrack Directory Name | COSMOS 252 DEB |
| Follow COSMOS 252 DEB | COSMOS 252 DEB Tracker |
| Pass predictions COSMOS 252 DEB | Pass predictions COSMOS 252 DEB |
| Orbit launches |
1968-11-01 (57 years ago)
|
| Days in orbit | 21175 |
| Country/organisation of origin | Commonwealth of Independent States (former USSR) (CIS) |
| Starting point | TYMSC (Baikonur Cosmodrome, Kazakhstan) |
| Perigee | 766 km |
| Apogee | 1956 km |
| Orbit slope (inclination) | 62.27° |
| Laps per day | 13 |
| Height COSMOS 252 DEB | 1375.77 km |
Additional information COSMOS 252 DEB
COSMOS 252 DEB, 3814 is space debris in LEO originally from a launch on Fri, 01 Nov 1968 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 252 DEB Date of exalting 01.11.1968y. Average height of ISS COSMOS 252 DEB hundred 1375.77 km. Average velocity COSMOS 252 DEB is 25822.93 km/h. Inclination COSMOS 252 DEB satellite 62.27°.TLE
Average velocity COSMOS 252 DEB
Average inclination COSMOS 252 DEB
Mean right ascension of the ascending node (RAAN) COSMOS 252 DEB
Mean argument of perigee COSMOS 252 DEB
Mean semi-major axis of the orbit COSMOS 252 DEB
Mean orbital eccentricity COSMOS 252 DEB
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