METEOSAT 4 AKM
Satellite information METEOSAT 4 AKM
| Spacetrack Directory Name | METEOSAT 4 AKM |
| Follow METEOSAT 4 AKM | METEOSAT 4 AKM Tracker |
| Pass predictions METEOSAT 4 AKM | Pass predictions METEOSAT 4 AKM |
| Orbit launches |
1989-03-06 (37 years ago)
|
| Days in orbit | 13713 |
| Country/organisation of origin | European Space Agency (ESA) |
| Starting point | FRGUI (Guiana Space Centre, French Guiana) |
| Perigee | 35205 km |
| Apogee | 36259 km |
| Orbit slope (inclination) | 10.88° |
| Laps per day | 1 |
| Height METEOSAT 4 AKM | 35747.97 km |
Additional information METEOSAT 4 AKM
METEOSAT 4 AKM, 20800 is space debris in GEO originally from a launch on Mon, 06 Mar 1989 UTC launched from the French Guiana (FRGUI). 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 METEOSAT 4 AKM Date of exalting 06.03.1989y. Average height of ISS METEOSAT 4 AKM hundred 35747.97 km. Average velocity METEOSAT 4 AKM is 11073.84 km/h. Inclination METEOSAT 4 AKM satellite 10.9°.TLE
Average velocity METEOSAT 4 AKM
Average inclination METEOSAT 4 AKM
Mean right ascension of the ascending node (RAAN) METEOSAT 4 AKM
Mean argument of perigee METEOSAT 4 AKM
Mean semi-major axis of the orbit METEOSAT 4 AKM
Mean orbital eccentricity METEOSAT 4 AKM
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