FENGYUN 1C DEB, 30326

Orbit data source: Space-Track

FENGYUN 1C DEB, 30326 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
30326, 1999-025AAM
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
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
Last TLE update: 1 day ago

TLE from 1 day ago
0 FENGYUN 1C DEB
1 30326U 99025AAM 25240.61991323  .00000165  00000-0  16722-3 0  9999
2 30326  98.6626 135.9774 0141284 319.8898  39.1896 13.85417150939861
Epoch: 2025-08-28T14:52Z
TLE epoch observation values (Epoch: 2025-08-28T14:52:40.503Z)
Latitude
0.00005°
Longitude
-64.27167°
Altitude
867.995 km
Speed
7.459 km/s
True Right ascension
09h 03m 54s
True Declination
0° 00' 00"
Sunlit
Object was in daylight 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
12:49:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,045.358 km
Perigee altitude
838.516 km
Semi-major axis
7,320.074 km
Eccentricity
0.01413
Inclination
98.6626°
RAAN
135.9774°
Arg. of periapsis
319.8898°
True anomaly
40.22676°
Mean anomaly
39.1896°
Eccentric anomaly
39.70675°
Mean motion
3.46553 °/min
Orbital period
103.88 mins
BSTAR
0.00016722
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