FENGYUN 1C DEB, 31016

Orbit data source: Space-Track

FENGYUN 1C DEB, 31016 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
31016, 1999-025BDJ
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: 15 hours ago

TLE from 15 hours ago
0 FENGYUN 1C DEB
1 31016U 99025BDJ 26071.04023513  .00000830  00000-0  31190-3 0  9998
2 31016  98.4330  89.2024 0112990  10.8894  49.8802 14.30648752987473
Epoch: 2026-03-12T00:57Z
TLE epoch observation values (Epoch: 2026-03-12T00:57:56.315Z)
Latitude
60.73244°
Longitude
-110.23354°
Altitude
748.243 km
Speed
7.513 km/s
True Right ascension
04h 55m 47s
True Declination
60° 35' 07"
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
20:01:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
867.649 km
Perigee altitude
705.738 km
Semi-major axis
7,164.831 km
Eccentricity
0.0113
Inclination
98.433°
RAAN
89.2024°
Arg. of periapsis
10.8894°
True anomaly
50.87935°
Mean anomaly
49.8802°
Eccentric anomaly
50.37887°
Mean motion
3.57877 °/min
Orbital period
100.59 mins
BSTAR
0.0003119
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