FENGYUN 1C DEB, 30660
Orbit data source: Space-Track
FENGYUN 1C DEB, 30660 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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30660 intel report (Beta)
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Edit Public Description
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: 2 days ago
TLE from 2 days ago
0 FENGYUN 1C DEB
1 30660U 99025APS 25350.08625294 .00004262 00000-0 40113-3 0 9997
2 30660 98.1391 86.6315 0136896 323.5173 159.4066 14.87578274 8343Epoch: 2025-12-16T02:04Z
TLE epoch observation values (Epoch: 2025-12-16T02:04:12.254Z)
Latitude
55.77124°
Longitude
162.674°
Altitude
704.466 km
Speed
7.461 km/s
True Right ascension
18h 34m 48s
True Declination
55° 36' 36"
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
16:16:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
698.108 km
Perigee altitude
506.983 km
Semi-major axis
6,980.683 km
Eccentricity
0.01369
Inclination
98.1391°
RAAN
86.6315°
Arg. of periapsis
323.5173°
True anomaly
159.94966°
Mean anomaly
159.4066°
Eccentric anomaly
159.67899°
Mean motion
3.72131 °/min
Orbital period
96.74 mins
BSTAR
0.00040113
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-12-17 18:27:44.612Z | 51.132° ENE | 2025-12-17 18:30:44.612Z | 94.017° ESE | 18.743° | 2025-12-17 18:33:44.612Z | 136.488° SSE |
| 7 mins | 2025-12-17 20:03:44.612Z | 348.997° N | 2025-12-17 20:06:44.612Z | 283.605° WNW | 33.812° | 2025-12-17 20:10:44.612Z | 220.138° SW |
| 6 mins | 2025-12-18 06:55:44.612Z | 192.601° SSW | 2025-12-18 06:57:44.612Z | 257.451° W | 39.283° | 2025-12-18 07:01:44.612Z | 337.531° 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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