P 76-5 DEB
Satellite information P 76-5 DEB - 0 P 76-5 DEB
| Spacetrack Directory Name | P 76-5 DEB |
| Alternative name | 0 P 76-5 DEB |
| Follow P 76-5 DEB | P 76-5 DEB Tracker |
| Pass predictions P 76-5 DEB | Pass predictions P 76-5 DEB |
| Orbit launches |
1976-05-22 (50 years ago)
|
| Days in orbit | 18362 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 958 km |
| Apogee | 1016 km |
| Orbit slope (inclination) | 99.86° |
| Laps per day | 14 |
| Height P 76-5 DEB | 999.04 km |
Additional information P 76-5 DEB
P 76-5 DEB, 59984 is space debris in SSO originally from an American launch on Sat, 22 May 1976 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 P 76-5 DEB Date of exalting 22.05.1976y. Average height of ISS P 76-5 DEB hundred 999.04 km. Average velocity P 76-5 DEB is 26473.62 km/h. Inclination P 76-5 DEB satellite 99.86°.TLE
Average velocity P 76-5 DEB
Average inclination P 76-5 DEB
Mean right ascension of the ascending node (RAAN) P 76-5 DEB
Mean argument of perigee P 76-5 DEB
Mean semi-major axis of the orbit P 76-5 DEB
Mean orbital eccentricity P 76-5 DEB
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