FENGYUN 1C DEB, 30266
Orbit data source: Space-Track
FENGYUN 1C DEB, 30266 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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30266 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
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 30266U 99025YB 25265.43311884 .00003304 00000-0 16935-2 0 9990
2 30266 99.0494 328.5679 0082047 294.4210 84.3814 14.14420420956401Epoch: 2025-09-22T10:23Z
TLE epoch observation values (Epoch: 2025-09-22T10:23:41.467Z)
Latitude
19.4843°
Longitude
167.89446°
Altitude
841.406 km
Speed
7.436 km/s
True Right ascension
21h 41m 25s
True Declination
19° 22' 40"
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
12:25:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
900.701 km
Perigee altitude
782.232 km
Semi-major axis
7,219.604 km
Eccentricity
0.0082
Inclination
99.0494°
RAAN
328.5679°
Arg. of periapsis
294.421°
True anomaly
85.31797°
Mean anomaly
84.3814°
Eccentric anomaly
84.8496°
Mean motion
3.53812 °/min
Orbital period
101.75 mins
BSTAR
0.0016935
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-24 03:11:17.368Z | 117.817° SE | 2025-09-24 03:15:17.368Z | 68.724° E | 24.065° | 2025-09-24 03:19:17.368Z | 15.131° NNE |
| 8 mins | 2025-09-24 04:52:17.368Z | 199.986° SSW | 2025-09-24 04:56:17.368Z | 275.416° WNW | 33.293° | 2025-09-24 05:00:17.368Z | 328.322° NNW |
| 10 mins | 2025-09-24 17:13:17.368Z | 15.016° NNE | 2025-09-24 17:17:17.368Z | 28.429° NE | 44.475° | 2025-09-24 17:23:17.368Z | 194.468° SSW |
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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