FENGYUN 1C DEB, 30561
Orbit data source: Space-Track
FENGYUN 1C DEB, 30561 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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30561 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Unknown
Mission
Spacecraft
Bus & Motor
Unknown
Mass
Unknown
Launch date (UTC)
Launch vehicle
Unknown
Launch site
Object type
Shape & HBR
Unknown shape, 0.1 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 FENGYUN 1C DEB
1 30561U 99025ALB 26087.66363740 .00000517 00000-0 30406-3 0 9997
2 30561 98.7286 91.8546 0059843 172.5180 250.8809 14.11416146984724Epoch: 2026-03-28T15:55Z
TLE epoch observation values (Epoch: 2026-03-28T15:55:38.271Z)
Latitude
61.58483°
Longitude
10.46811°
Altitude
879.439 km
Speed
7.411 km/s
True Right ascension
05h 01m 49s
True Declination
61° 26' 35"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
09:56:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
894.966 km
Perigee altitude
808.435 km
Semi-major axis
7,229.838 km
Eccentricity
0.00598
Inclination
98.7286°
RAAN
91.8546°
Arg. of periapsis
172.518°
True anomaly
250.23457°
Mean anomaly
250.8809°
Eccentric anomaly
250.55758°
Mean motion
3.53061 °/min
Orbital period
101.97 mins
BSTAR
0.00030406
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Other satellites on launch #25 in the year 1999 (1999-05-10 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.FENGYUN 1C DEB Visibility forecast
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Span | Click to sort rows by Start time (UTC) header in descending order | Start Az. | Max El. time (UTC) | Max El. Az. | Max El. | End time (UTC) | End Az. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-03-29 12:37:41.028Z | 26.096° NE | 2026-03-29 12:42:41.028Z | 100.896° ESE | 36.309° | 2026-03-29 12:47:41.028Z | 173.297° S |
| 6 mins | 2026-03-29 14:20:41.028Z | 330.288° NNW | 2026-03-29 14:22:41.028Z | 302.53° NW | 20.232° | 2026-03-29 14:26:41.028Z | 250.262° W |
| 9 mins | 2026-03-30 00:04:41.028Z | 160.547° S | 2026-03-30 00:08:41.028Z | 116.33° SE | 44.516° | 2026-03-30 00:13:41.028Z | 348.763° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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