FENGYUN 1C DEB
Satellite information FENGYUN 1C DEB
| Spacetrack Directory Name | FENGYUN 1C DEB |
| Follow FENGYUN 1C DEB | FENGYUN 1C DEB Tracker |
| Pass predictions FENGYUN 1C DEB | Pass predictions FENGYUN 1C DEB |
| Orbit launches |
1999-05-10 (27 years ago)
|
| Days in orbit | 9973 |
| Country/organisation of origin | Chiny (PRC) |
| Starting point | TAISC (Taiyuan Space Center, China) |
| Perigee | 844 km |
| Apogee | 1189 km |
| Orbit slope (inclination) | 98.85° |
| Laps per day | 14 |
| Height FENGYUN 1C DEB | 1009.72 km |
Additional information FENGYUN 1C DEB
FENGYUN 1C DEB, 29917 is space debris in SSO originally from a launch on Mon, 10 May 1999 UTC launched from the Taiyaun Space Center, China (TSC). Fengyun 1C debris stems from the Chinese weather satellite Fengyun-1C, which was intentionally destroyed by a Chinese anti-satellite missile in 2007. This event dramatically increased the amount of space debris, with thousands of trackable fragments posing hazards to satellites and human spaceflight. The Fengyun 1C debris cloud has become a focal point in discussions about space sustainability and the need for international regulations to prevent the creation of new debris.
satellite FENGYUN 1C DEB Date of exalting 10.05.1999y. Average height of ISS FENGYUN 1C DEB hundred 1009.72 km. Average velocity FENGYUN 1C DEB is 26454.35 km/h. Inclination FENGYUN 1C DEB satellite 98.86°.TLE
Average velocity FENGYUN 1C DEB
Average inclination FENGYUN 1C DEB
Mean right ascension of the ascending node (RAAN) FENGYUN 1C DEB
Mean argument of perigee FENGYUN 1C DEB
Mean semi-major axis of the orbit FENGYUN 1C DEB
Mean orbital eccentricity FENGYUN 1C DEB
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