HIMAWARI 4 (GMS 4)
Satellite information HIMAWARI 4 (GMS 4)
| Spacetrack Directory Name | HIMAWARI 4 (GMS 4) |
| Follow HIMAWARI 4 (GMS 4) | HIMAWARI 4 (GMS 4) Tracker |
| Pass predictions HIMAWARI 4 (GMS 4) | Pass predictions HIMAWARI 4 (GMS 4) |
| Orbit launches |
1989-09-05 (37 years ago)
|
| Days in orbit | 13563 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 36407 km |
| Apogee | 36810 km |
| Orbit slope (inclination) | 14.73° |
| Laps per day | 1 |
| Height HIMAWARI 4 (GMS 4) | 36608.63 km |
Additional information HIMAWARI 4 (GMS 4)
HIMAWARI 4 (GMS 4), 20217 is a payload satellite owned by NASDA (JP) in GEO that was launched on Tue, 05 Sep 1989 UTC via an H-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 HIMAWARI 4 (GMS 4) Date of exalting 05.09.1989y. Average height of ISS HIMAWARI 4 (GMS 4) hundred 36608.63 km. Average velocity HIMAWARI 4 (GMS 4) is 10962.62 km/h. Inclination HIMAWARI 4 (GMS 4) satellite 14.75°.TLE
Average velocity HIMAWARI 4 (GMS 4)
Average inclination HIMAWARI 4 (GMS 4)
Mean right ascension of the ascending node (RAAN) HIMAWARI 4 (GMS 4)
Mean argument of perigee HIMAWARI 4 (GMS 4)
Mean semi-major axis of the orbit HIMAWARI 4 (GMS 4)
Mean orbital eccentricity HIMAWARI 4 (GMS 4)
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