FENGYUN 1C DEB, 37686

Orbit data source: Space-Track

FENGYUN 1C DEB, 37686 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.

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Identifier
37686, 1999-025ELB
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 37686U 99025ELB 26021.28796170  .00000614  00000-0  82803-3 0  9991
2 37686  99.0198  40.1981 0394897 304.0987  69.8585 13.35405175611555
Epoch: 2026-01-21T06:54Z
TLE epoch observation values (Epoch: 2026-01-21T06:54:39.890Z)
Latitude
18.03439°
Longitude
172.92708°
Altitude
1,037.148 km
Speed
7.379 km/s
True Right ascension
02h 29m 00s
True Declination
17° 56' 14"
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
13:00:26
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,419.972 km
Perigee altitude
827.479 km
Semi-major axis
7,501.862 km
Eccentricity
0.03949
Inclination
99.0198°
RAAN
40.1981°
Arg. of periapsis
304.0987°
True anomaly
74.17626°
Mean anomaly
69.8585°
Eccentric anomaly
72.01048°
Mean motion
3.34033 °/min
Orbital period
107.77 mins
BSTAR
0.00082803
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