HIMAWARI 1 (GMS 1)
Satellite information HIMAWARI 1 (GMS 1)
| Spacetrack Directory Name | HIMAWARI 1 (GMS 1) |
| Follow HIMAWARI 1 (GMS 1) | HIMAWARI 1 (GMS 1) Tracker |
| Pass predictions HIMAWARI 1 (GMS 1) | Pass predictions HIMAWARI 1 (GMS 1) |
| Orbit launches |
1977-07-14 (49 years ago)
|
| Days in orbit | 17954 |
| Country/organisation of origin | Japonia (JPN) |
| Starting point | AFETR (Kennedy Space Center/Cape Canaveral, USA) |
| Perigee | 36011 km |
| Apogee | 36142 km |
| Orbit slope (inclination) | 6.32° |
| Laps per day | 1 |
| Height HIMAWARI 1 (GMS 1) | 36075.7 km |
Additional information HIMAWARI 1 (GMS 1)
HIMAWARI 1 (GMS 1), 10143 is a payload satellite owned by NASDA (JP) in GEO that was launched on Thu, 14 Jul 1977 UTC via a DELTA 2914 launch vehicle from the Air Force Eastern Test Range (AFETR). 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 1 (GMS 1) Date of exalting 14.07.1977y. Average height of ISS HIMAWARI 1 (GMS 1) hundred 36075.7 km. Average velocity HIMAWARI 1 (GMS 1) is 11031.11 km/h. Inclination HIMAWARI 1 (GMS 1) satellite 6.35°.TLE
Average velocity HIMAWARI 1 (GMS 1)
Average inclination HIMAWARI 1 (GMS 1)
Mean right ascension of the ascending node (RAAN) HIMAWARI 1 (GMS 1)
Mean argument of perigee HIMAWARI 1 (GMS 1)
Mean semi-major axis of the orbit HIMAWARI 1 (GMS 1)
Mean orbital eccentricity HIMAWARI 1 (GMS 1)
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