COBE DEB
Satellite information COBE DEB
| Spacetrack Directory Name | COBE DEB |
| Follow COBE DEB | COBE DEB Tracker |
| Pass predictions COBE DEB | Pass predictions COBE DEB |
| Orbit launches |
1989-11-18 (36 years ago)
|
| Days in orbit | 13432 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | Here |
| Perigee | 879 km |
| Apogee | 882 km |
| Orbit slope (inclination) | 98.93° |
| Laps per day | 14 |
| Height COBE DEB | 889.19 km |
Additional information COBE DEB
COBE DEB, 20328 is space debris in SSO originally from a launch on Sat, 18 Nov 1989 UTC launched 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 COBE DEB Date of exalting 18.11.1989y. Average height of ISS COBE DEB hundred 889.19 km. Average velocity COBE DEB is 26672.87 km/h. Inclination COBE DEB satellite 98.93°.TLE
Average velocity COBE DEB
Average inclination COBE DEB
Mean right ascension of the ascending node (RAAN) COBE DEB
Mean argument of perigee COBE DEB
Mean semi-major axis of the orbit COBE DEB
Mean orbital eccentricity COBE DEB
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