OV1-10 R/B
Satellite information OV1-10 R/B
| Spacetrack Directory Name | OV1-10 R/B |
| Follow OV1-10 R/B | OV1-10 R/B Tracker |
| Pass predictions OV1-10 R/B | Pass predictions OV1-10 R/B |
| Orbit launches |
1966-12-11 (59 years ago)
|
| Days in orbit | 21816 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | Here |
| Perigee | 585 km |
| Apogee | 667 km |
| Orbit slope (inclination) | 93.39° |
| Laps per day | 15 |
| Height OV1-10 R/B | 623.83 km |
Additional information OV1-10 R/B
OV1-10 R/B, 2621 is space debris in LEO originally from a launch on Sun, 11 Dec 1966 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 OV1-10 R/B Date of exalting 11.12.1966y. Average height of ISS OV1-10 R/B hundred 623.83 km. Average velocity OV1-10 R/B is 27173.54 km/h. Inclination OV1-10 R/B satellite 93.39°.TLE
Average velocity OV1-10 R/B
Average inclination OV1-10 R/B
Mean right ascension of the ascending node (RAAN) OV1-10 R/B
Mean argument of perigee OV1-10 R/B
Mean semi-major axis of the orbit OV1-10 R/B
Mean orbital eccentricity OV1-10 R/B
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