P/L 153 DEB
Satellite information P/L 153 DEB
| Spacetrack Directory Name | P/L 153 DEB |
| Follow P/L 153 DEB | P/L 153 DEB Tracker |
| Pass predictions P/L 153 DEB | Pass predictions P/L 153 DEB |
| Orbit launches |
1967-05-31 (59 years ago)
|
| Days in orbit | 21645 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 823 km |
| Apogee | 834 km |
| Orbit slope (inclination) | 69.96° |
| Laps per day | 14 |
| Height P/L 153 DEB | 825.48 km |
Additional information P/L 153 DEB
P/L 153 DEB, 19245 is space debris in LEO originally from a launch on Wed, 31 May 1967 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/L 153 DEB Date of exalting 31.05.1967y. Average height of ISS P/L 153 DEB hundred 825.48 km. Average velocity P/L 153 DEB is 26791.15 km/h. Inclination P/L 153 DEB satellite 69.96°.TLE
Average velocity P/L 153 DEB
Average inclination P/L 153 DEB
Mean right ascension of the ascending node (RAAN) P/L 153 DEB
Mean argument of perigee P/L 153 DEB
Mean semi-major axis of the orbit P/L 153 DEB
Mean orbital eccentricity P/L 153 DEB
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