FENGYUN 1A
Satellite information FENGYUN 1A - FY-1A
| Spacetrack Directory Name | FENGYUN 1A |
| Alternative name | FY-1A |
| Follow FENGYUN 1A | FENGYUN 1A Tracker |
| Pass predictions FENGYUN 1A | Pass predictions FENGYUN 1A |
| Orbit launches |
1988-09-06 (37 years ago)
|
| Days in orbit | 13870 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TAISC (Taiyuan Space Center, China) |
| Perigee | 872 km |
| Apogee | 894 km |
| Orbit slope (inclination) | 99.02° |
| Laps per day | 14 |
| Height FENGYUN 1A | 893.36 km |
Additional information FENGYUN 1A
FENGYUN 1A, 19467 is a payload satellite owned by CNMSC (CN) in SSO that was launched on Tue, 06 Sep 1988 UTC via a CHANG ZHENG 4 launch vehicle from the Taiyaun Space Center, China (TSC). 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 FENGYUN 1A Date of exalting 06.09.1988y. Average height of ISS FENGYUN 1A hundred 893.36 km. Average velocity FENGYUN 1A is 26665.29 km/h. Inclination FENGYUN 1A satellite 99.02°.TLE
Average velocity FENGYUN 1A
Average inclination FENGYUN 1A
Mean right ascension of the ascending node (RAAN) FENGYUN 1A
Mean argument of perigee FENGYUN 1A
Mean semi-major axis of the orbit FENGYUN 1A
Mean orbital eccentricity FENGYUN 1A
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