FENGYUN 1B
Satellite information FENGYUN 1B - FY-1B
| Spacetrack Directory Name | FENGYUN 1B |
| Alternative name | FY-1B |
| Follow FENGYUN 1B | FENGYUN 1B Tracker |
| Pass predictions FENGYUN 1B | Pass predictions FENGYUN 1B |
| Orbit launches |
1990-09-03 (35 years ago)
|
| Days in orbit | 13143 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TAISC (Taiyuan Space Center, China) |
| Perigee | 872 km |
| Apogee | 896 km |
| Orbit slope (inclination) | 98.98° |
| Laps per day | 14 |
| Height FENGYUN 1B | 894.53 km |
Additional information FENGYUN 1B
FENGYUN 1B, 20788 is a payload satellite owned by CNMSC (CN) in SSO that was launched on Mon, 03 Sep 1990 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 1B Date of exalting 03.09.1990y. Average height of ISS FENGYUN 1B hundred 894.53 km. Average velocity FENGYUN 1B is 26663.15 km/h. Inclination FENGYUN 1B satellite 98.98°.TLE
Average velocity FENGYUN 1B
Average inclination FENGYUN 1B
Mean right ascension of the ascending node (RAAN) FENGYUN 1B
Mean argument of perigee FENGYUN 1B
Mean semi-major axis of the orbit FENGYUN 1B
Mean orbital eccentricity FENGYUN 1B
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