ATLAS 75E R/B
Satellite information ATLAS 75E R/B
| Spacetrack Directory Name | ATLAS 75E R/B |
| Follow ATLAS 75E R/B | ATLAS 75E R/B Tracker |
| Pass predictions ATLAS 75E R/B | Pass predictions ATLAS 75E R/B |
| Orbit launches |
1983-07-14 (43 years ago)
|
| Days in orbit | 15751 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 941 km |
| Apogee | 20586 km |
| Orbit slope (inclination) | 64.3° |
| Laps per day | 4 |
| Height ATLAS 75E R/B | 13342.71 km |
Additional information ATLAS 75E R/B
ATLAS 75E R/B, 14190 is space debris in HEO originally from a launch on Thu, 14 Jul 1983 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 ATLAS 75E R/B Date of exalting 14.07.1983y. Average height of ISS ATLAS 75E R/B hundred 13342.71 km. Average velocity ATLAS 75E R/B is 15971.07 km/h. Inclination ATLAS 75E R/B satellite 64.3°.TLE
Average velocity ATLAS 75E R/B
Average inclination ATLAS 75E R/B
Mean right ascension of the ascending node (RAAN) ATLAS 75E R/B
Mean argument of perigee ATLAS 75E R/B
Mean semi-major axis of the orbit ATLAS 75E R/B
Mean orbital eccentricity ATLAS 75E R/B
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