FENGYUN 1C DEB, 30125

Orbit data source: Space-Track

FENGYUN 1C DEB, 30125 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
30125, 1999-025SE
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, 0.069 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 30125U 99025SE  26267.52479260  .00002242  00000-0  54964-3 0  9995
2 30125  98.7296   9.7030 0335503 234.0031 189.0832 14.24602173  9870
Epoch: 2026-09-24T12:35Z
TLE epoch observation values (Epoch: 2026-09-24T12:35:42.080Z)
Latitude
61.34585°
Longitude
161.18316°
Altitude
1,058.653 km
Speed
7.206 km/s
True Right ascension
23h 33m 52s
True Declination
61° 12' 24"
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
14:06:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,048.042 km
Perigee altitude
565.916 km
Semi-major axis
7,185.116 km
Eccentricity
0.03355
Inclination
98.7296°
RAAN
9.703°
Arg. of periapsis
234.0031°
True anomaly
188.50044°
Mean anomaly
189.0832°
Eccentric anomaly
188.78947°
Mean motion
3.56363 °/min
Orbital period
101.02 mins
BSTAR
0.00054964
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