FENGYUN 1C DEB, 41832

Orbit data source: Space-Track

FENGYUN 1C DEB, 41832 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.

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Identifier
41832, 1999-025EYK
Orbit
SSO
Last TLE update
21 hours ago
Origin
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1999-05-10 (26 years ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history

TLE from 21 hours ago
0 FENGYUN 1C DEB
1 41832U 99025EYK 25199.11001444  .00001926  00000-0  86218-3 0  9990
2 41832  98.7404 264.1905 0053551 294.0023  65.5555 14.22986100452508
Epoch: 2025-07-18T02:38Z
TLE epoch observation values (Epoch: 2025-07-18T02:38:25.247Z)
Latitude
-0°
Longitude
-71.58088°
Altitude
802.417 km
Speed
7.46 km/s
True Right ascension
17h 36m 45s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
19.5115°
Longitude
112.39411°
Altitude
842.996 km
Speed
7.42 km/s
Apparent Right ascension
03h 41m 34s
Apparent Declination
-10° 34' 55"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:26:25
Azimuth
290.378° WNW
Elevation
-37.919°
Doppler factor
1
Orbital elements
Apogee altitude
850.934 km
Perigee altitude
773.921 km
Semi-major axis
7,190.565 km
Eccentricity
0.00536
Inclination
98.7404°
RAAN
264.1905°
Arg. of periapsis
294.0023°
True anomaly
66.11569°
Mean anomaly
65.5555°
Eccentric anomaly
65.83544°
Mean motion
3.55958 °/min
Orbital period
101.14 mins
BSTAR
0.00086218
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