FENGYUN 1C DEB, 31910

Orbit data source: Space-Track

FENGYUN 1C DEB, 31910 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
31910, 1999-025CLM
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: 4 weeks ago

TLE from 4 weeks ago
0 FENGYUN 1C DEB
1 31910U 99025CLM 26034.27001156  .00007163  00000-0  13993-2 0  9990
2 31910  97.6633  55.6434 0225377 353.1022   6.7086 14.48232089651290
Epoch: 2026-02-03T06:28Z
TLE epoch observation values (Epoch: 2026-02-03T06:28:48.998Z)
Latitude
-0°
Longitude
-175.01412°
Altitude
575.297 km
Speed
7.657 km/s
True Right ascension
03h 42m 34s
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
12:30:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
888.667 km
Perigee altitude
568.332 km
Semi-major axis
7,106.636 km
Eccentricity
0.02254
Inclination
97.6633°
RAAN
55.6434°
Arg. of periapsis
353.1022°
True anomaly
7.01897°
Mean anomaly
6.7086°
Eccentric anomaly
6.8629°
Mean motion
3.62282 °/min
Orbital period
99.37 mins
BSTAR
0.0013993
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|