FENGYUN 1C DEB, 30403

Orbit data source: Space-Track

FENGYUN 1C DEB, 30403 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
30403, 1999-025ADS
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 shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history
Last TLE update: 6 hours ago

TLE from 6 hours ago
0 FENGYUN 1C DEB
1 30403U 99025ADS 25289.14557012  .00007005  00000-0  31616-2 0  9997
2 30403  99.0617   6.0936 0079594 186.3517 173.6657 14.20771233959887
Epoch: 2025-10-16T03:29Z
TLE epoch observation values (Epoch: 2025-10-16T03:29:37.258Z)
Latitude
-0.00001°
Longitude
-71.22113°
Altitude
882.631 km
Speed
7.382 km/s
True Right ascension
00h 24m 22s
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
04:25:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
877.212 km
Perigee altitude
762.628 km
Semi-major axis
7,198.057 km
Eccentricity
0.00796
Inclination
99.0617°
RAAN
6.0936°
Arg. of periapsis
186.3517°
True anomaly
173.76534°
Mean anomaly
173.6657°
Eccentric anomaly
173.71562°
Mean motion
3.55402 °/min
Orbital period
101.29 mins
BSTAR
0.0031616
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