FENGYUN 1C DEB, 31284

Orbit data source: Space-Track

FENGYUN 1C DEB, 31284 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
31284, 1999-025BNS
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: 17 hours ago

TLE from 17 hours ago
0 FENGYUN 1C DEB
1 31284U 99025BNS 26263.16325859  .00000359  00000-0  26246-3 0  9991
2 31284  99.7312  19.2368 0141656  21.2316 339.4645 13.98423520990951
Epoch: 2026-09-20T03:55Z
TLE epoch observation values (Epoch: 2026-09-20T03:55:05.542Z)
Latitude
0.00002°
Longitude
-38.59768°
Altitude
805.737 km
Speed
7.5 km/s
True Right ascension
01h 16m 56s
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
14:02:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
999.547 km
Perigee altitude
793.448 km
Semi-major axis
7,274.634 km
Eccentricity
0.01417
Inclination
99.7312°
RAAN
19.2368°
Arg. of periapsis
21.2316°
True anomaly
338.8855°
Mean anomaly
339.4645°
Eccentric anomaly
339.17597°
Mean motion
3.49805 °/min
Orbital period
102.91 mins
BSTAR
0.00026246
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