ATLAS H R/B
Satellite information ATLAS H R/B
| Spacetrack Directory Name | ATLAS H R/B |
| Follow ATLAS H R/B | ATLAS H R/B Tracker |
| Pass predictions ATLAS H R/B | Pass predictions ATLAS H R/B |
| Orbit launches |
1986-02-09 (40 years ago)
|
| Days in orbit | 14810 |
| Country/organisation of origin | USA (US) |
| Starting point | AFWTR (Vandenberg Air Force Base, USA) |
| Perigee | 678 km |
| Apogee | 1341 km |
| Orbit slope (inclination) | 63.34° |
| Laps per day | 14 |
| Height ATLAS H R/B | 995.33 km |
Additional information ATLAS H R/B
ATLAS H R/B, 16592 is space debris in LEO originally from a launch on Sun, 09 Feb 1986 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 H R/B Date of exalting 09.02.1986y. Average height of ISS ATLAS H R/B hundred 995.33 km. Average velocity ATLAS H R/B is 26481 km/h. Inclination ATLAS H R/B satellite 63.34°.TLE
Average velocity ATLAS H R/B
Average inclination ATLAS H R/B
Mean right ascension of the ascending node (RAAN) ATLAS H R/B
Mean argument of perigee ATLAS H R/B
Mean semi-major axis of the orbit ATLAS H R/B
Mean orbital eccentricity ATLAS H R/B
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