ATLAS 2A R/B
Satellite information ATLAS 2A R/B
| Spacetrack Directory Name | ATLAS 2A R/B |
| Follow ATLAS 2A R/B | ATLAS 2A R/B Tracker |
| Pass predictions ATLAS 2A R/B | Pass predictions ATLAS 2A R/B |
| Orbit launches |
1998-01-29 (28 years ago)
|
| Days in orbit | 10448 |
| Country/organisation of origin | USA (US) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 1288 km |
| Apogee | 37990 km |
| Orbit slope (inclination) | 62.13° |
| Laps per day | 2 |
| Height ATLAS 2A R/B | 25524.71 km |
Additional information ATLAS 2A R/B
ATLAS 2A R/B, 25149 is space debris in HEO originally from a launch on Thu, 29 Jan 1998 UTC launched from the Air Force Eastern Test Range (AFETR). 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 2A R/B Date of exalting 29.01.1998y. Average height of ISS ATLAS 2A R/B hundred 25524.71 km. Average velocity ATLAS 2A R/B is 12340.56 km/h. Inclination ATLAS 2A R/B satellite 62.13°.TLE
Average velocity ATLAS 2A R/B
Average inclination ATLAS 2A R/B
Mean right ascension of the ascending node (RAAN) ATLAS 2A R/B
Mean argument of perigee ATLAS 2A R/B
Mean semi-major axis of the orbit ATLAS 2A R/B
Mean orbital eccentricity ATLAS 2A R/B
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