OV1-5 DEB
Satellite information OV1-5 DEB
| Spacetrack Directory Name | OV1-5 DEB |
| Follow OV1-5 DEB | OV1-5 DEB Tracker |
| Pass predictions OV1-5 DEB | Pass predictions OV1-5 DEB |
| Orbit launches |
1966-03-30 (60 years ago)
|
| Days in orbit | 22072 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| WWW | Here |
| Perigee | 784 km |
| Apogee | 833 km |
| Orbit slope (inclination) | 144.61° |
| Laps per day | 15 |
| Height OV1-5 DEB | 704.4 km |
Additional information OV1-5 DEB
OV1-5 DEB, 5361 is space debris in LEO originally from a launch on Wed, 30 Mar 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 OV1-5 DEB Date of exalting 30.03.1966y. Average height of ISS OV1-5 DEB hundred 704.4 km. Average velocity OV1-5 DEB is 27022.7 km/h. Inclination OV1-5 DEB satellite 144.61°.TLE
Average velocity OV1-5 DEB
Average inclination OV1-5 DEB
Mean right ascension of the ascending node (RAAN) OV1-5 DEB
Mean argument of perigee OV1-5 DEB
Mean semi-major axis of the orbit OV1-5 DEB
Mean orbital eccentricity OV1-5 DEB
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