ATLAS 55E R/B
Satellite information ATLAS 55E R/B
| Spacetrack Directory Name | ATLAS 55E R/B |
| Follow ATLAS 55E R/B | ATLAS 55E R/B Tracker |
| Pass predictions ATLAS 55E R/B | Pass predictions ATLAS 55E R/B |
| Orbit launches |
1985-10-09 (40 years ago)
|
| Days in orbit | 14933 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 1024 km |
| Apogee | 20259 km |
| Orbit slope (inclination) | 64.31° |
| Laps per day | 4 |
| Height ATLAS 55E R/B | 13141.61 km |
Additional information ATLAS 55E R/B
ATLAS 55E R/B, 16137 is space debris in HEO originally from a launch on Wed, 09 Oct 1985 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 55E R/B Date of exalting 09.10.1985y. Average height of ISS ATLAS 55E R/B hundred 13141.61 km. Average velocity ATLAS 55E R/B is 16075.99 km/h. Inclination ATLAS 55E R/B satellite 64.3°.TLE
Average velocity ATLAS 55E R/B
Average inclination ATLAS 55E R/B
Mean right ascension of the ascending node (RAAN) ATLAS 55E R/B
Mean argument of perigee ATLAS 55E R/B
Mean semi-major axis of the orbit ATLAS 55E R/B
Mean orbital eccentricity ATLAS 55E R/B
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