FENGYUN 1C DEB, 29736

Orbit data source: Space-Track

FENGYUN 1C DEB, 29736 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
29736, 1999-025AA
Orbit
SSO
Country
Flag of CNCN / PRC
Related business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1999-05-10 (26 years ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 FENGYUN 1C DEB
1 29736U 99025AA  25260.54553023  .00000479  00000-0  11158-2 0  9992
2 29736  99.4116  96.4185 0727053  23.2751  34.3179 12.57312562854611
Epoch: 2025-09-17T13:05Z
TLE epoch observation values (Epoch: 2025-09-17T13:05:33.811Z)
Latitude
61.30085°
Longitude
-114.2209°
Altitude
989.626 km
Speed
7.574 km/s
True Right ascension
05h 15m 33s
True Declination
61° 09' 37"
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
10:54:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,999.247 km
Perigee altitude
863.651 km
Semi-major axis
7,809.586 km
Eccentricity
0.07271
Inclination
99.4116°
RAAN
96.4185°
Arg. of periapsis
23.2751°
True anomaly
39.38815°
Mean anomaly
34.3179°
Eccentric anomaly
36.81408°
Mean motion
3.14486 °/min
Orbital period
114.47 mins
BSTAR
0.0011158
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
|