FENGYUN 1C DEB, 30082

Orbit data source: Space-Track

FENGYUN 1C DEB, 30082 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
30082, 1999-025QK
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, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 14 hours ago

TLE from 14 hours ago
0 FENGYUN 1C DEB
1 30082U 99025QK  26087.13389078  .00032321  00000-0  13084-2 0  9999
2 30082  98.8249  37.3853 0059387 171.2382 188.9902 15.22983644 28933
Epoch: 2026-03-28T03:12Z
TLE epoch observation values (Epoch: 2026-03-28T03:12:48.163Z)
Latitude
-0°
Longitude
163.62612°
Altitude
540.239 km
Speed
7.57 km/s
True Right ascension
02h 29m 32s
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
22:35:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
534.686 km
Perigee altitude
453.064 km
Semi-major axis
6,872.012 km
Eccentricity
0.00594
Inclination
98.8249°
RAAN
37.3853°
Arg. of periapsis
171.2382°
True anomaly
188.88463°
Mean anomaly
188.9902°
Eccentric anomaly
188.93734°
Mean motion
3.80993 °/min
Orbital period
94.49 mins
BSTAR
0.0013084
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