OV1-21 R/B
Satellite information OV1-21 R/B - OV1-21
| Spacetrack Directory Name | OV1-21 R/B |
| Alternative name | OV1-21 |
| Follow OV1-21 R/B | OV1-21 R/B Tracker |
| Pass predictions OV1-21 R/B | Pass predictions OV1-21 R/B |
| 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 | 773 km |
| Apogee | 894 km |
| Orbit slope (inclination) | 87.63° |
| Laps per day | 14 |
| Height OV1-21 R/B | 843.73 km |
Additional information OV1-21 R/B
OV1-21 R/B, 5397 is space debris in LEO originally from a launch on Sat, 07 Aug 1971 UTC via an ATLAS F launch vehicle 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 OV1-21 R/B Date of exalting 07.08.1971y. Average height of ISS OV1-21 R/B hundred 843.73 km. Average velocity OV1-21 R/B is 26756.56 km/h. Inclination OV1-21 R/B satellite 87.63°.TLE
Average velocity OV1-21 R/B
Average inclination OV1-21 R/B
Mean right ascension of the ascending node (RAAN) OV1-21 R/B
Mean argument of perigee OV1-21 R/B
Mean semi-major axis of the orbit OV1-21 R/B
Mean orbital eccentricity OV1-21 R/B
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