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
Last TLE update
9 hours ago
Origin
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
1999-05-10 (26 years ago)
Launch vehicle
Unknown
Launch site
Taiyaun Space Center, China (TSC)
Object type
Payload
Rocket body
Debris
Shape & HBR
Unknown
Radar Cross Section
Small (<0.1 m²)

Expand to show TLE details & history

TLE from 9 hours ago
0 FENGYUN 1C DEB *
1 46993U 99025EZT 25199.60743955  .00000160  00000-0  18214-3 0  9997
2 46993  98.7083 331.9064 0262720 329.2698  44.4140 13.69000653582445
Epoch: 2025-07-18T14:34Z
TLE epoch observation values (Epoch: 2025-07-18T14:34:42.777Z)
Latitude
15.63331°
Longitude
174.12814°
Altitude
869.354 km
Speed
7.487 km/s
True Right ascension
21h 57m 51s
True Declination
15° 32' 44"
Sunlit
Object was in full shadow at epoch
Visualization orbit readout
Latitude
50.73077°
Longitude
166.16777°
Altitude
983.157 km
Speed
7.379 km/s
Apparent Right ascension
22h 54m 33s
Apparent Declination
10° 13' 38"
Sunlit
Object is in daylight
Visualization observer readout
Local Sidereal Time
12:18:43
Azimuth
25.965° NE
Elevation
-36.196°
Doppler factor
1
Orbital elements
Apogee altitude
1,194.234 km
Perigee altitude
806.537 km
Semi-major axis
7,378.522 km
Eccentricity
0.02627
Inclination
98.7083°
RAAN
331.9064°
Arg. of periapsis
329.2698°
True anomaly
46.57095°
Mean anomaly
44.414°
Eccentric anomaly
45.48741°
Mean motion
3.42444 °/min
Orbital period
105.13 mins
BSTAR
0.00018214
Loading maneuver chart data...
Loading SW <> Apogee altitude chart data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
Loading historical data...
|