HIMAWARI 3 (GMS 3)
Satellite information HIMAWARI 3 (GMS 3)
| Spacetrack Directory Name | HIMAWARI 3 (GMS 3) |
| Follow HIMAWARI 3 (GMS 3) | HIMAWARI 3 (GMS 3) Tracker |
| Pass predictions HIMAWARI 3 (GMS 3) | Pass predictions HIMAWARI 3 (GMS 3) |
| Orbit launches |
1984-08-02 (42 years ago)
|
| Days in orbit | 15373 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | TANSC (Tanegashima Space Center, Japan) |
| Perigee | 35875 km |
| Apogee | 35942 km |
| Orbit slope (inclination) | 10.51° |
| Laps per day | 1 |
| Height HIMAWARI 3 (GMS 3) | 35910.97 km |
Additional information HIMAWARI 3 (GMS 3)
HIMAWARI 3 (GMS 3), 15152 is a payload satellite owned by NASDA (JP) in GEO that was launched on Thu, 02 Aug 1984 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 3 (GMS 3) Date of exalting 02.08.1984y. Average height of ISS HIMAWARI 3 (GMS 3) hundred 35910.97 km. Average velocity HIMAWARI 3 (GMS 3) is 11052.66 km/h. Inclination HIMAWARI 3 (GMS 3) satellite 10.53°.TLE
Average velocity HIMAWARI 3 (GMS 3)
Average inclination HIMAWARI 3 (GMS 3)
Mean right ascension of the ascending node (RAAN) HIMAWARI 3 (GMS 3)
Mean argument of perigee HIMAWARI 3 (GMS 3)
Mean semi-major axis of the orbit HIMAWARI 3 (GMS 3)
Mean orbital eccentricity HIMAWARI 3 (GMS 3)
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