FENGYUN 1C DEB, 40690

Orbit data source: Space-Track

FENGYUN 1C DEB, 40690 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
40690, 1999-025EWW
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: 1 month ago

TLE from 1 month ago
0 FENGYUN 1C DEB
1 40690U 99025EWW 26175.33357660  .00000476  00000-0  36891-3 0  9995
2 40690  99.3998 219.4001 0092102 343.3120  16.5016 13.95910210640768
Epoch: 2026-06-24T08:00Z
TLE epoch observation values (Epoch: 2026-06-24T08:00:21.018Z)
Latitude
Longitude
-173.17977°
Altitude
846.546 km
Speed
7.462 km/s
True Right ascension
14h 37m 36s
True Declination
0° 00' 00"
Sunlit
Object was in full shadow 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
20:38:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
972.298 km
Perigee altitude
838.135 km
Semi-major axis
7,283.353 km
Eccentricity
0.00921
Inclination
99.3998°
RAAN
219.4001°
Arg. of periapsis
343.312°
True anomaly
16.80472°
Mean anomaly
16.5016°
Eccentric anomaly
16.65283°
Mean motion
3.49177 °/min
Orbital period
103.1 mins
BSTAR
0.00036891
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