FENGYUN 1C DEB, 37464

Orbit data source: Space-Track

FENGYUN 1C DEB, 37464 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
37464, 1999-025EJJ
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: 5 days ago

TLE from 5 days ago
0 FENGYUN 1C DEB
1 37464U 99025EJJ 26131.65819609  .00001980  00000-0  17643-2 0  9997
2 37464 102.7100 101.4275 0451757 148.5156 214.3863 13.48112278629412
Epoch: 2026-05-11T15:47Z
TLE epoch observation values (Epoch: 2026-05-11T15:47:48.142Z)
Latitude
0.00001°
Longitude
-4.96686°
Altitude
1,364.55 km
Speed
7.039 km/s
True Right ascension
06h 45m 42s
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
12:25:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,413.462 km
Perigee altitude
739.909 km
Semi-major axis
7,454.822 km
Eccentricity
0.04518
Inclination
102.71°
RAAN
101.4275°
Arg. of periapsis
148.5156°
True anomaly
211.59412°
Mean anomaly
214.3863°
Eccentric anomaly
212.97742°
Mean motion
3.372 °/min
Orbital period
106.76 mins
BSTAR
0.0017643
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
|