AYAME 1 DEB
Satellite information AYAME 1 DEB - AYAME DEB
| Spacetrack Directory Name | AYAME 1 DEB |
| Alternative name | AYAME DEB |
| Follow AYAME 1 DEB | AYAME 1 DEB Tracker |
| Pass predictions AYAME 1 DEB | Pass predictions AYAME 1 DEB |
| Orbit launches |
1979-02-06 (47 years ago)
|
| Days in orbit | 17377 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| WWW | Here |
| Perigee | 12641 km |
| Apogee | 34263 km |
| Orbit slope (inclination) | 9.78° |
| Laps per day | 2 |
| Height AYAME 1 DEB | 25573.92 km |
Additional information AYAME 1 DEB
AYAME 1 DEB, 38682 is space debris in HEO originally from a launch on Tue, 06 Feb 1979 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 1 DEB Date of exalting 06.02.1979y. Average height of ISS AYAME 1 DEB hundred 25573.92 km. Average velocity AYAME 1 DEB is 12662.33 km/h. Inclination AYAME 1 DEB satellite 9.8°.TLE
Average velocity AYAME 1 DEB
Average inclination AYAME 1 DEB
Mean right ascension of the ascending node (RAAN) AYAME 1 DEB
Mean argument of perigee AYAME 1 DEB
Mean semi-major axis of the orbit AYAME 1 DEB
Mean orbital eccentricity AYAME 1 DEB
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