FENGYUN 1C DEB, 30365

Orbit data source: Space-Track

FENGYUN 1C DEB, 30365 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
30365, 1999-025ACC
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: 16 hours ago

TLE from 16 hours ago
0 FENGYUN 1C DEB
1 30365U 99025ACC 26145.95291419  .00000479  00000-0  21644-3 0  9990
2 30365  98.6277 141.0984 0166678 358.0470  55.0604 14.19439283999423
Epoch: 2026-05-25T22:52Z
TLE epoch observation values (Epoch: 2026-05-25T22:52:11.786Z)
Latitude
53.88809°
Longitude
-97.42315°
Altitude
768.641 km
Speed
7.51 km/s
True Right ascension
08h 36m 38s
True Declination
53° 43' 28"
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
00:12:38
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
944.454 km
Perigee altitude
704.353 km
Semi-major axis
7,202.541 km
Eccentricity
0.01667
Inclination
98.6277°
RAAN
141.0984°
Arg. of periapsis
358.047°
True anomaly
56.64482°
Mean anomaly
55.0604°
Eccentric anomaly
55.85073°
Mean motion
3.5507 °/min
Orbital period
101.39 mins
BSTAR
0.00021644
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