FENGYUN 1C DEB, 30382

Orbit data source: Space-Track

FENGYUN 1C DEB, 30382 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
30382, 1999-025ACV
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: 17 hours ago

TLE from 17 hours ago
0 FENGYUN 1C DEB
1 30382U 99025ACV 26045.05445608  .00001849  00000-0  70301-3 0  9996
2 30382  98.4926  86.4899 0155620 171.1939 254.5782 14.25649523984375
Epoch: 2026-02-14T01:18Z
TLE epoch observation values (Epoch: 2026-02-14T01:18:25.005Z)
Latitude
62.89122°
Longitude
-94.06403°
Altitude
848.431 km
Speed
7.418 km/s
True Right ascension
04h 38m 29s
True Declination
62° 45' 12"
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
20:41:16
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
915.209 km
Perigee altitude
691.69 km
Semi-major axis
7,181.586 km
Eccentricity
0.01556
Inclination
98.4926°
RAAN
86.4899°
Arg. of periapsis
171.1939°
True anomaly
252.86824°
Mean anomaly
254.5782°
Eccentric anomaly
253.7223°
Mean motion
3.56626 °/min
Orbital period
100.95 mins
BSTAR
0.00070301
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