FENGYUN 1C DEB, 31660

Orbit data source: Space-Track

FENGYUN 1C DEB, 31660 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
31660, 1999-025CBS
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 days ago

TLE from 4 days ago
0 FENGYUN 1C DEB
1 31660U 99025CBS 26118.23284287  .00001144  00000-0  45584-3 0  9994
2 31660  98.5105 120.9714 0102063 140.1752 220.6977 14.27607355 98631
Epoch: 2026-04-28T05:35Z
TLE epoch observation values (Epoch: 2026-04-28T05:35:17.623Z)
Latitude
-0.00006°
Longitude
-179.06312°
Altitude
858.54 km
Speed
7.394 km/s
True Right ascension
08h 03m 53s
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
01:45:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
870.109 km
Perigee altitude
723.648 km
Semi-major axis
7,175.015 km
Eccentricity
0.01021
Inclination
98.5105°
RAAN
120.9714°
Arg. of periapsis
140.1752°
True anomaly
219.9424°
Mean anomaly
220.6977°
Eccentric anomaly
220.31932°
Mean motion
3.57116 °/min
Orbital period
100.81 mins
BSTAR
0.00045584
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|