AYAME 2 (ECS-2)
Satellite information AYAME 2 (ECS-2) - AYAME-2 (ECS-B)
| Spacetrack Directory Name | AYAME 2 (ECS-2) |
| Alternative name | AYAME-2 (ECS-B) |
| Follow AYAME 2 (ECS-2) | AYAME 2 (ECS-2) Tracker |
| Pass predictions AYAME 2 (ECS-2) | Pass predictions AYAME 2 (ECS-2) |
| 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) |
| Perigee | 10029 km |
| Apogee | 35281 km |
| Orbit slope (inclination) | 9.62° |
| Laps per day | 2 |
| Height AYAME 2 (ECS-2) | 25518 km |
Additional information AYAME 2 (ECS-2)
AYAME 2 (ECS-2), 11715 is a payload satellite owned by NASDA (JP) in HEO that was launched on Fri, 22 Feb 1980 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 2 (ECS-2) Date of exalting 22.02.1980y. Average height of ISS AYAME 2 (ECS-2) hundred 25518 km. Average velocity AYAME 2 (ECS-2) is 12640.37 km/h. Inclination AYAME 2 (ECS-2) satellite 9.61°.TLE
Average velocity AYAME 2 (ECS-2)
Average inclination AYAME 2 (ECS-2)
Mean right ascension of the ascending node (RAAN) AYAME 2 (ECS-2)
Mean argument of perigee AYAME 2 (ECS-2)
Mean semi-major axis of the orbit AYAME 2 (ECS-2)
Mean orbital eccentricity AYAME 2 (ECS-2)
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