FENGYUN 1C DEB, 37079

Orbit data source: Space-Track

FENGYUN 1C DEB, 37079 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
37079, 1999-025EFP
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: 17 hours ago

TLE from 17 hours ago
0 FENGYUN 1C DEB
1 37079U 99025EFP 25347.11767411  .00026542  00000-0  55286-2 0  9997
2 37079  98.8571 122.1025 0011724 142.0543 218.1483 14.59894284646213
Epoch: 2025-12-13T02:49Z
TLE epoch observation values (Epoch: 2025-12-13T02:49:27.043Z)
Latitude
-0.00002°
Longitude
-2.30972°
Altitude
703.004 km
Speed
7.501 km/s
True Right ascension
08h 08m 24s
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
18:08:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
698.916 km
Perigee altitude
682.341 km
Semi-major axis
7,068.765 km
Eccentricity
0.00117
Inclination
98.8571°
RAAN
122.1025°
Arg. of periapsis
142.0543°
True anomaly
218.06541°
Mean anomaly
218.1483°
Eccentric anomaly
218.10685°
Mean motion
3.65198 °/min
Orbital period
98.58 mins
BSTAR
0.0055286
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|