FENGYUN 1C DEB, 32323

Orbit data source: Space-Track

FENGYUN 1C DEB, 32323 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
32323, 1999-025CXQ
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1999-05-10 (27 years ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown shape, 0.050 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 2 days ago

TLE from 2 days ago
0 FENGYUN 1C DEB
1 32323U 99025CXQ 26267.16538986  .00002620  00000-0  16768-2 0  9997
2 32323  98.5839  36.7003 0152891 134.3076 227.0745 13.98606417642572
Epoch: 2026-09-24T03:58Z
TLE epoch observation values (Epoch: 2026-09-24T03:58:09.683Z)
Latitude
-0.00005°
Longitude
-25.84611°
Altitude
978.199 km
Speed
7.324 km/s
True Right ascension
02h 26m 48s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
N/A
Visualization observer readout
Local Sidereal Time
17:22:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,007.017 km
Perigee altitude
784.593 km
Semi-major axis
7,273.942 km
Eccentricity
0.01529
Inclination
98.5839°
RAAN
36.7003°
Arg. of periapsis
134.3076°
True anomaly
225.80821°
Mean anomaly
227.0745°
Eccentric anomaly
226.43971°
Mean motion
3.49855 °/min
Orbital period
102.9 mins
BSTAR
0.0016768
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