FENGYUN 1C DEB, 35123

Orbit data source: Space-Track

FENGYUN 1C DEB, 35123 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
35123, 1999-025DLB
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: 2 days ago

TLE from 2 days ago
0 FENGYUN 1C DEB
1 35123U 99025DLB 26166.79706044  .00000895  00000-0  40106-3 0  9993
2 35123  99.1227   1.5957 0047597 266.5595  93.0138 14.24638229637082
Epoch: 2026-06-15T19:07Z
TLE epoch observation values (Epoch: 2026-06-15T19:07:46.022Z)
Latitude
0.00004°
Longitude
170.57564°
Altitude
814.578 km
Speed
7.445 km/s
True Right ascension
00h 06m 22s
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
20:55:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
841.08 km
Perigee altitude
772.683 km
Semi-major axis
7,185.019 km
Eccentricity
0.00476
Inclination
99.1227°
RAAN
1.5957°
Arg. of periapsis
266.5595°
True anomaly
93.55829°
Mean anomaly
93.0138°
Eccentric anomaly
93.28606°
Mean motion
3.5637 °/min
Orbital period
101.02 mins
BSTAR
0.00040106
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|