DECAYED

FENGYUN 1C DEB, 30532 (Decayed)

Orbit data source: Space-Track

FENGYUN 1C DEB, 30532 was 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
30532, 1999-025AJW
Orbit
Decayed
Country
Flag of CNCN / PRC
Related business
Manufacturer
Unknown
Mission
Decayed 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 30532U 99025AJW 26010.90643109  .06579795  00000-0  25341-1 0  9993
2 30532  96.9423  59.7939 0001026 167.2242 192.9055 15.82942114981379
Epoch: 2026-01-10T21:45Z
TLE epoch observation values (Epoch: 2026-01-10T21:45:15.646Z)
Latitude
0.00004°
Longitude
-16.9464°
Altitude
325.984 km
Speed
7.712 km/s
True Right ascension
03h 59m 10s
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
13:24:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
319.675 km
Perigee altitude
318.301 km
Semi-major axis
6,697.125 km
Eccentricity
0.0001
Inclination
96.9423°
RAAN
59.7939°
Arg. of periapsis
167.2242°
True anomaly
192.90287°
Mean anomaly
192.9055°
Eccentric anomaly
192.90419°
Mean motion
3.96014 °/min
Orbital period
90.91 mins
BSTAR
0.025341
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|