DECAYED

FENGYUN 1C DEB, 31505 (Decayed)

Orbit data source: Space-Track

FENGYUN 1C DEB, 31505 was 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.

Not visible in the next 10 days
Identifier
31505, 1999-025BWU
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
Manufacturer
Unknown
Mission
Decayed 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: 5 months ago

TLE from 5 months ago
0 FENGYUN 1C DEB
1 31505U 99025BWU 25187.80436107  .02012309  00000-0  16618-1 0  9991
2 31505 101.8729 133.1395 0021013 146.8856 213.3708 15.66931004944044
Epoch: 2025-07-06T19:18Z
TLE epoch observation values (Epoch: 2025-07-06T19:18:16.796Z)
Latitude
-0.00002°
Longitude
-81.45327°
Altitude
382.526 km
Speed
7.674 km/s
True Right ascension
08h 52m 33s
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
18:01:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
379.015 km
Perigee altitude
350.677 km
Semi-major axis
6,742.983 km
Eccentricity
0.0021
Inclination
101.8729°
RAAN
133.1395°
Arg. of periapsis
146.8856°
True anomaly
213.23864°
Mean anomaly
213.3708°
Eccentric anomaly
213.30469°
Mean motion
3.91981 °/min
Orbital period
91.84 mins
BSTAR
0.016618
Loading maneuver chart data...
Computing Atmospheric mass density...

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