FENGYUN 1C DEB, 32340

Orbit data source: Space-Track

FENGYUN 1C DEB, 32340 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
32340, 1999-025CYH
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, 0.055 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 32340U 99025CYH 26295.08638443  .00013429  00000-0  16549-2 0  9993
2 32340  98.9638 341.9835 0028945  29.5707 330.7132 14.82768949 17890
Epoch: 2026-10-22T02:04Z
TLE epoch observation values (Epoch: 2026-10-22T02:04:23.614Z)
Latitude
-0.0001°
Longitude
-79.64121°
Altitude
605.931 km
Speed
7.566 km/s
True Right ascension
22h 47m 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
04:06:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
637.935 km
Perigee altitude
597.436 km
Semi-major axis
6,995.822 km
Eccentricity
0.00289
Inclination
98.9638°
RAAN
341.9835°
Arg. of periapsis
29.5707°
True anomaly
330.55043°
Mean anomaly
330.7132°
Eccentric anomaly
330.63187°
Mean motion
3.70924 °/min
Orbital period
97.05 mins
BSTAR
0.0016549
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|