FENGYUN 1C DEB, 30327

Orbit data source: Space-Track

FENGYUN 1C DEB, 30327 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
30327, 1999-025AAN
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: 23 hours ago

TLE from 23 hours ago
0 FENGYUN 1C DEB
1 30327U 99025AAN 25245.65993050  .00008398  00000-0  39161-2 0  9995
2 30327  98.4466 144.9536 0122246  74.9787 351.3187 14.16766402950116
Epoch: 2025-09-02T15:50Z
TLE epoch observation values (Epoch: 2025-09-02T15:50:17.995Z)
Latitude
64.80798°
Longitude
-92.9698°
Altitude
760.285 km
Speed
7.525 km/s
True Right ascension
08h 26m 36s
True Declination
64° 40' 31"
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
06:32:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
921.618 km
Perigee altitude
745.3 km
Semi-major axis
7,211.596 km
Eccentricity
0.01222
Inclination
98.4466°
RAAN
144.9536°
Arg. of periapsis
74.9787°
True anomaly
351.10402°
Mean anomaly
351.3187°
Eccentric anomaly
351.21169°
Mean motion
3.54402 °/min
Orbital period
101.58 mins
BSTAR
0.0039161
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