HIMAWARI 7
Satellite information HIMAWARI 7 - HIMAWARI-7 (MTSAT-2)
| Spacetrack Directory Name | HIMAWARI 7 |
| Alternative name | HIMAWARI-7 (MTSAT-2) |
| Follow HIMAWARI 7 | HIMAWARI 7 Tracker |
| Pass predictions HIMAWARI 7 | Pass predictions HIMAWARI 7 |
| Orbit launches |
2006-02-18 (20 years ago)
|
| Days in orbit | 7502 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Categories | |
| Perigee | 36112 km |
| Apogee | 36140 km |
| Orbit slope (inclination) | 5.97° |
| Laps per day | 1 |
| Orbit | GEO |
| Height HIMAWARI 7 | 36124.48 km |
Additional information HIMAWARI 7
HIMAWARI 7, 28937 is a Japanese payload satellite in GEO that was launched on Sat, 18 Feb 2006 UTC via an H-IIA 2024 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 7 Date of exalting 18.02.2006y. Average height of ISS HIMAWARI 7 hundred 36124.48 km. Average velocity HIMAWARI 7 is 11024.83 km/h. Inclination HIMAWARI 7 satellite 5.95°.TLE
Average velocity HIMAWARI 7
Average inclination HIMAWARI 7
Mean right ascension of the ascending node (RAAN) HIMAWARI 7
Mean argument of perigee HIMAWARI 7
Mean semi-major axis of the orbit HIMAWARI 7
Mean orbital eccentricity HIMAWARI 7
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