FENGYUN 1C DEB, 30573

Orbit data source: Space-Track

FENGYUN 1C DEB, 30573 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
30573, 1999-025ALP
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: 11 hours ago

TLE from 11 hours ago
0 FENGYUN 1C DEB
1 30573U 99025ALP 26087.71779039  .00002638  00000-0  13490-2 0  9997
2 30573  99.2160 133.8521 0085994 336.7788 145.7610 14.14601812976955
Epoch: 2026-03-28T17:13Z
TLE epoch observation values (Epoch: 2026-03-28T17:13:37.089Z)
Latitude
55.89173°
Longitude
-116.89932°
Altitude
904.439 km
Speed
7.379 km/s
True Right ascension
21h 50m 33s
True Declination
55° 44' 06"
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
09:59:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
902.936 km
Perigee altitude
778.778 km
Semi-major axis
7,218.994 km
Eccentricity
0.0086
Inclination
99.216°
RAAN
133.8521°
Arg. of periapsis
336.7788°
True anomaly
146.31055°
Mean anomaly
145.761°
Eccentric anomaly
146.03626°
Mean motion
3.53857 °/min
Orbital period
101.74 mins
BSTAR
0.001349
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
|