HIMAWARI 6
Satellite information HIMAWARI 6 - HIMAWARI-6 (MTSAT-1R)
| Spacetrack Directory Name | HIMAWARI 6 |
| Alternative name | HIMAWARI-6 (MTSAT-1R) |
| Follow HIMAWARI 6 | HIMAWARI 6 Tracker |
| Pass predictions HIMAWARI 6 | Pass predictions HIMAWARI 6 |
| Orbit launches |
2005-02-26 (21 years ago)
|
| Days in orbit | 7859 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 36101 km |
| Apogee | 36241 km |
| Orbit slope (inclination) | 9.56° |
| Laps per day | 1 |
| Height HIMAWARI 6 | 36172.05 km |
Additional information HIMAWARI 6
HIMAWARI 6, 28622 is a payload satellite owned by JAXA (JP) in GEO that was launched on Sat, 26 Feb 2005 UTC via an H-IIA 2022 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 6 Date of exalting 26.02.2005y. Average height of ISS HIMAWARI 6 hundred 36172.05 km. Average velocity HIMAWARI 6 is 11018.66 km/h. Inclination HIMAWARI 6 satellite 9.54°.TLE
Average velocity HIMAWARI 6
Average inclination HIMAWARI 6
Mean right ascension of the ascending node (RAAN) HIMAWARI 6
Mean argument of perigee HIMAWARI 6
Mean semi-major axis of the orbit HIMAWARI 6
Mean orbital eccentricity HIMAWARI 6
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