GOES 2 AKM
Satellite information GOES 2 AKM
| Spacetrack Directory Name | GOES 2 AKM |
| Follow GOES 2 AKM | GOES 2 AKM Tracker |
| Pass predictions GOES 2 AKM | Pass predictions GOES 2 AKM |
| Orbit launches |
1977-06-16 (49 years ago)
|
| Days in orbit | 17982 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 34788 km |
| Apogee | 36623 km |
| Orbit slope (inclination) | 3.89° |
| Laps per day | 1 |
| Height GOES 2 AKM | 35702.76 km |
Additional information GOES 2 AKM
GOES 2 AKM, 20799 is space debris in GEO originally from a launch on Thu, 16 Jun 1977 UTC launched from the Air Force Eastern Test Range (AFETR). 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 GOES 2 AKM Date of exalting 16.06.1977y. Average height of ISS GOES 2 AKM hundred 35702.76 km. Average velocity GOES 2 AKM is 11080.57 km/h. Inclination GOES 2 AKM satellite 3.93°.TLE
Average velocity GOES 2 AKM
Average inclination GOES 2 AKM
Mean right ascension of the ascending node (RAAN) GOES 2 AKM
Mean argument of perigee GOES 2 AKM
Mean semi-major axis of the orbit GOES 2 AKM
Mean orbital eccentricity GOES 2 AKM
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