FENGYUN 1C DEB, 30572

Orbit data source: Space-Track

FENGYUN 1C DEB, 30572 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
30572, 1999-025ALN
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: 10 hours ago

TLE from 10 hours ago
0 FENGYUN 1C DEB
1 30572U 99025ALN 26063.01623352  .00000667  00000-0  40858-3 0  9998
2 30572  98.7625  95.4334 0022811  65.2775 324.5064 14.09005002979066
Epoch: 2026-03-04T00:23Z
TLE epoch observation values (Epoch: 2026-03-04T00:23:22.576Z)
Latitude
29.30088°
Longitude
-77.13377°
Altitude
852.965 km
Speed
7.436 km/s
True Right ascension
06h 01m 59s
True Declination
29° 09' 23"
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
14:00:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
876.465 km
Perigee altitude
843.444 km
Semi-major axis
7,238.091 km
Eccentricity
0.00228
Inclination
98.7625°
RAAN
95.4334°
Arg. of periapsis
65.2775°
True anomaly
324.35428°
Mean anomaly
324.5064°
Eccentric anomaly
324.43037°
Mean motion
3.52458 °/min
Orbital period
102.14 mins
BSTAR
0.00040858
Loading maneuver chart data...
Computing Atmospheric mass density...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...

Documentation

Showing up to 5 results
|