AYAME 1 (ECS 1)
Satellite information AYAME 1 (ECS 1) - AYAME (ECS)
| Spacetrack Directory Name | AYAME 1 (ECS 1) |
| Alternative name | AYAME (ECS) |
| Follow AYAME 1 (ECS 1) | AYAME 1 (ECS 1) Tracker |
| Pass predictions AYAME 1 (ECS 1) | Pass predictions AYAME 1 (ECS 1) |
| 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) |
| Perigee | 12623 km |
| Apogee | 34264 km |
| Orbit slope (inclination) | 9.49° |
| Laps per day | 2 |
| Height AYAME 1 (ECS 1) | 25420.09 km |
Additional information AYAME 1 (ECS 1)
AYAME 1 (ECS 1), 11261 is a payload satellite owned by NASDA (JP) in HEO that was launched on Tue, 06 Feb 1979 UTC via an N-1 launch vehicle from the Tanegashima Space Center (TNSTA). Payloads include a variety of satellites, spacecraft, and rockets equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
satellite AYAME 1 (ECS 1) Date of exalting 06.02.1979y. Average height of ISS AYAME 1 (ECS 1) hundred 25420.09 km. Average velocity AYAME 1 (ECS 1) is 12721.79 km/h. Inclination AYAME 1 (ECS 1) satellite 9.52°.TLE
Average velocity AYAME 1 (ECS 1)
Average inclination AYAME 1 (ECS 1)
Mean right ascension of the ascending node (RAAN) AYAME 1 (ECS 1)
Mean argument of perigee AYAME 1 (ECS 1)
Mean semi-major axis of the orbit AYAME 1 (ECS 1)
Mean orbital eccentricity AYAME 1 (ECS 1)
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