HIMAWARI 2 (GMS 2)
Satellite information HIMAWARI 2 (GMS 2)
| Spacetrack Directory Name | HIMAWARI 2 (GMS 2) |
| Follow HIMAWARI 2 (GMS 2) | HIMAWARI 2 (GMS 2) Tracker |
| Pass predictions HIMAWARI 2 (GMS 2) | Pass predictions HIMAWARI 2 (GMS 2) |
| Orbit launches |
1981-08-10 (45 years ago)
|
| Days in orbit | 16461 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 35954 km |
| Apogee | 36027 km |
| Orbit slope (inclination) | 7.82° |
| Laps per day | 1 |
| Height HIMAWARI 2 (GMS 2) | 35987.63 km |
Additional information HIMAWARI 2 (GMS 2)
HIMAWARI 2 (GMS 2), 12677 is a payload satellite owned by NASDA (JP) in GEO that was launched on Mon, 10 Aug 1981 UTC via an N-2 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 HIMAWARI 2 (GMS 2) Date of exalting 10.08.1981y. Average height of ISS HIMAWARI 2 (GMS 2) hundred 35987.63 km. Average velocity HIMAWARI 2 (GMS 2) is 11042.66 km/h. Inclination HIMAWARI 2 (GMS 2) satellite 7.84°.TLE
Average velocity HIMAWARI 2 (GMS 2)
Average inclination HIMAWARI 2 (GMS 2)
Mean right ascension of the ascending node (RAAN) HIMAWARI 2 (GMS 2)
Mean argument of perigee HIMAWARI 2 (GMS 2)
Mean semi-major axis of the orbit HIMAWARI 2 (GMS 2)
Mean orbital eccentricity HIMAWARI 2 (GMS 2)
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