FENGYUN 1C DEB, 30110

Orbit data source: Space-Track

FENGYUN 1C DEB, 30110 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
30110, 1999-025RP
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 30110U 99025RP  25345.87226532  .00000268  00000-0  34694-3 0  9999
2 30110  98.9077  94.7621 0267643 355.3212   4.5434 13.56223894935038
Epoch: 2025-12-11T20:56Z
TLE epoch observation values (Epoch: 2025-12-11T20:56:03.723Z)
Latitude
-0.00005°
Longitude
59.92459°
Altitude
854.099 km
Speed
7.524 km/s
True Right ascension
06h 19m 02s
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
09:29:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,245.419 km
Perigee altitude
847.978 km
Semi-major axis
7,424.835 km
Eccentricity
0.02676
Inclination
98.9077°
RAAN
94.7621°
Arg. of periapsis
355.3212°
True anomaly
4.79472°
Mean anomaly
4.5434°
Eccentric anomaly
4.6682°
Mean motion
3.39245 °/min
Orbital period
106.12 mins
BSTAR
0.00034694
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