OV1-20/OV1-21 AKM
Satellite information OV1-20/OV1-21 AKM - 1971-067 AKM
| Spacetrack Directory Name | OV1-20/OV1-21 AKM |
| Alternative name | 1971-067 AKM |
| Follow OV1-20/OV1-21 AKM | OV1-20/OV1-21 AKM Tracker |
| Pass predictions OV1-20/OV1-21 AKM | Pass predictions OV1-20/OV1-21 AKM |
| Orbit launches |
1971-08-07 (55 years ago)
|
| Days in orbit | 20163 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | Here |
| Perigee | 726 km |
| Apogee | 808 km |
| Orbit slope (inclination) | 87.61° |
| Laps per day | 14 |
| Height OV1-20/OV1-21 AKM | 762.57 km |
Additional information OV1-20/OV1-21 AKM
OV1-20/OV1-21 AKM, 5395 is space debris in LEO originally from a launch on Sat, 07 Aug 1971 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 OV1-20/OV1-21 AKM Date of exalting 07.08.1971y. Average height of ISS OV1-20/OV1-21 AKM hundred 762.57 km. Average velocity OV1-20/OV1-21 AKM is 26908.25 km/h. Inclination OV1-20/OV1-21 AKM satellite 87.61°.TLE
Average velocity OV1-20/OV1-21 AKM
Average inclination OV1-20/OV1-21 AKM
Mean right ascension of the ascending node (RAAN) OV1-20/OV1-21 AKM
Mean argument of perigee OV1-20/OV1-21 AKM
Mean semi-major axis of the orbit OV1-20/OV1-21 AKM
Mean orbital eccentricity OV1-20/OV1-21 AKM
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