LES 2 AKM
Satellite information LES 2 AKM
| Spacetrack Directory Name | LES 2 AKM |
| Follow LES 2 AKM | LES 2 AKM Tracker |
| Pass predictions LES 2 AKM | Pass predictions LES 2 AKM |
| Orbit launches |
1965-05-06 (61 years ago)
|
| Days in orbit | 22408 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 2776 km |
| Apogee | 14800 km |
| Orbit slope (inclination) | 32.2° |
| Laps per day | 5 |
| Height LES 2 AKM | 9976.56 km |
Additional information LES 2 AKM
LES 2 AKM, 2529 is space debris in HEO originally from a launch on Thu, 06 May 1965 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 LES 2 AKM Date of exalting 06.05.1965y. Average height of ISS LES 2 AKM hundred 9976.56 km. Average velocity LES 2 AKM is 17718.5 km/h. Inclination LES 2 AKM satellite 32.2°.TLE
Average velocity LES 2 AKM
Average inclination LES 2 AKM
Mean right ascension of the ascending node (RAAN) LES 2 AKM
Mean argument of perigee LES 2 AKM
Mean semi-major axis of the orbit LES 2 AKM
Mean orbital eccentricity LES 2 AKM
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