FENGYUN 1C DEB, 30912
Orbit data source: Space-Track
FENGYUN 1C DEB, 30912 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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30912 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: 12 hours ago
TLE from 12 hours ago
0 FENGYUN 1C DEB
1 30912U 99025AZA 26095.85877004 .00014721 00000-0 13725-2 0 9996
2 30912 98.9880 318.0213 0055276 93.1633 267.5909 14.93190439 11022Epoch: 2026-04-05T20:36Z
TLE epoch observation values (Epoch: 2026-04-05T20:36:37.731Z)
Latitude
-0.00004°
Longitude
174.70594°
Altitude
592.831 km
Speed
7.563 km/s
True Right ascension
21h 12m 05s
True Declination
0° 00' 00"
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
14:16:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
623.56 km
Perigee altitude
546.581 km
Semi-major axis
6,963.208 km
Eccentricity
0.00553
Inclination
98.988°
RAAN
318.0213°
Arg. of periapsis
93.1633°
True anomaly
266.95824°
Mean anomaly
267.5909°
Eccentric anomaly
267.27455°
Mean motion
3.73533 °/min
Orbital period
96.38 mins
BSTAR
0.0013725
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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 | 2026-04-06 14:26:10.743Z | 146.548° SSE | 2026-04-06 14:29:10.743Z | 67.002° ENE | 39.356° | 2026-04-06 14:32:10.743Z | 358.134° N |
| 7 mins | 2026-04-07 03:43:10.743Z | 13.889° NNE | 2026-04-07 03:47:10.743Z | 194.501° SSW | 44.896° | 2026-04-07 03:50:10.743Z | 195.031° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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