FENGYUN 1C DEB, 33728

Orbit data source: Space-Track

FENGYUN 1C DEB, 33728 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.

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Identifier
33728, 1999-025DHR
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, 0.072 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)

Expand to show TLE details & history
Last TLE update: 1 day ago

TLE from 1 day ago
0 FENGYUN 1C DEB
1 33728U 99025DHR 26298.23347531  .00003582  00000-0  26917-3 0  9999
2 33728  98.9606  43.8633 0138539 275.1029  83.4389 14.96071671 30285
Epoch: 2026-10-25T05:36Z
TLE epoch observation values (Epoch: 2026-10-25T05:36:12.266Z)
Latitude
-0.00004°
Longitude
-73.81605°
Altitude
572.364 km
Speed
7.58 km/s
True Right ascension
02h 55m 27s
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
01:07:23
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
672.461 km
Perigee altitude
479.774 km
Semi-major axis
6,954.255 km
Eccentricity
0.01385
Inclination
98.9606°
RAAN
43.8633°
Arg. of periapsis
275.1029°
True anomaly
85.01897°
Mean anomaly
83.4389°
Eccentric anomaly
84.22865°
Mean motion
3.74255 °/min
Orbital period
96.19 mins
BSTAR
0.00026917
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