FENGYUN 1C DEB, 30492

Orbit data source: Space-Track

FENGYUN 1C DEB, 30492 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.

Loading next visibility...
Identifier
30492, 1999-025AHE
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 30492U 99025AHE 25352.70141945  .00010100  00000-0  23757-2 0  9999
2 30492 102.3249  12.7004 0094339  47.0212 313.8829 14.51996911969812
Epoch: 2025-12-18T16:50Z
TLE epoch observation values (Epoch: 2025-12-18T16:50:02.640Z)
Latitude
-0.00001°
Longitude
32.63625°
Altitude
675.862 km
Speed
7.543 km/s
True Right ascension
00h 50m 48s
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
08:52:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
783.39 km
Perigee altitude
649.53 km
Semi-major axis
7,094.597 km
Eccentricity
0.00943
Inclination
102.3249°
RAAN
12.7004°
Arg. of periapsis
47.0212°
True anomaly
313.09733°
Mean anomaly
313.8829°
Eccentric anomaly
313.49076°
Mean motion
3.63205 °/min
Orbital period
99.12 mins
BSTAR
0.0023757
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|