FENGYUN 1C DEB, 36160

Orbit data source: Space-Track

FENGYUN 1C DEB, 36160 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
36160, 1999-025DSH
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: 2 weeks ago

TLE from 2 weeks ago
0 FENGYUN 1C DEB
1 36160U 99025DSH 26239.28624391  .00000428  00000-0  22661-3 0  9992
2 36160  98.1380  62.8014 0135170 126.2278 235.1480 14.13457630636904
Epoch: 2026-08-27T06:52Z
TLE epoch observation values (Epoch: 2026-08-27T06:52:11.473Z)
Latitude
-0.00003°
Longitude
-15.77347°
Altitude
907.193 km
Speed
7.369 km/s
True Right ascension
04h 11m 12s
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
10:31:09
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
942.335 km
Perigee altitude
747.073 km
Semi-major axis
7,222.841 km
Eccentricity
0.01352
Inclination
98.138°
RAAN
62.8014°
Arg. of periapsis
126.2278°
True anomaly
233.88916°
Mean anomaly
235.148°
Eccentric anomaly
234.51736°
Mean motion
3.53575 °/min
Orbital period
101.82 mins
BSTAR
0.00022661
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|