AYAME 2 DEB
Satellite information AYAME 2 DEB
| Spacetrack Directory Name | AYAME 2 DEB |
| Follow AYAME 2 DEB | AYAME 2 DEB Tracker |
| Pass predictions AYAME 2 DEB | Pass predictions AYAME 2 DEB |
| Orbit launches |
1980-02-22 (46 years ago)
|
| Days in orbit | 16996 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| WWW | Here |
| Perigee | 9420 km |
| Apogee | 35503 km |
| Orbit slope (inclination) | 10.07° |
| Laps per day | 2 |
| Height AYAME 2 DEB | 25311.75 km |
Additional information AYAME 2 DEB
AYAME 2 DEB, 38684 is space debris in HEO originally from a launch on Fri, 22 Feb 1980 UTC launched from the Tanegashima Space Center (TNSTA). 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 AYAME 2 DEB Date of exalting 22.02.1980y. Average height of ISS AYAME 2 DEB hundred 25311.75 km. Average velocity AYAME 2 DEB is 12704.61 km/h. Inclination AYAME 2 DEB satellite 10.07°.TLE
Average velocity AYAME 2 DEB
Average inclination AYAME 2 DEB
Mean right ascension of the ascending node (RAAN) AYAME 2 DEB
Mean argument of perigee AYAME 2 DEB
Mean semi-major axis of the orbit AYAME 2 DEB
Mean orbital eccentricity AYAME 2 DEB
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