FENGYUN 1C DEB *, 46993

Orbit data source: Space-Track

FENGYUN 1C DEB *, 46993 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
46993, 1999-025EZT
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: 3 days ago

TLE from 3 days ago
0 FENGYUN 1C DEB *
1 46993U 99025EZT 25310.14136887  .00000290  00000-0  29658-3 0  9999
2 46993  98.7219  72.0085 0263579  36.5631 139.8154 13.69106095597560
Epoch: 2025-11-06T03:23Z
TLE epoch observation values (Epoch: 2025-11-06T03:23:34.270Z)
Latitude
1.59813°
Longitude
155.75576°
Altitude
1,156.165 km
Speed
7.201 km/s
True Right ascension
16h 49m 00s
True Declination
1° 35' 21"
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
11:52:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,194.479 km
Perigee altitude
805.534 km
Semi-major axis
7,378.144 km
Eccentricity
0.02636
Inclination
98.7219°
RAAN
72.0085°
Arg. of periapsis
36.5631°
True anomaly
141.71607°
Mean anomaly
139.8154°
Eccentric anomaly
140.77049°
Mean motion
3.4247 °/min
Orbital period
105.12 mins
BSTAR
0.00029658
Loading maneuver chart data...
Computing Atmospheric mass density...

Documentation

Showing up to 5 results
|