FENGYUN 1C DEB, 30380
Orbit data source: Space-Track
FENGYUN 1C DEB, 30380 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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30380 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 FENGYUN 1C DEB
1 30380U 99025ACT 26302.15229646 .00000375 00000-0 89924-4 0 9998
2 30380 98.8725 13.0890 0175157 331.7572 27.4207 14.51342797 42113Epoch: 2026-10-29T03:39Z
TLE epoch observation values (Epoch: 2026-10-29T03:39:18.414Z)
Latitude
0.00004°
Longitude
-79.22856°
Altitude
614.29 km
Speed
7.61 km/s
True Right ascension
00h 52m 21s
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
17:16:21
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
842.69 km
Perigee altitude
594.089 km
Semi-major axis
7,096.527 km
Eccentricity
0.01752
Inclination
98.8725°
RAAN
13.089°
Arg. of periapsis
331.7572°
True anomaly
28.3633°
Mean anomaly
27.4207°
Eccentric anomaly
27.89015°
Mean motion
3.63057 °/min
Orbital period
99.16 mins
BSTAR
0.000089924
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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 | 2026-10-30 04:35:53.731Z | 152.042° SSE | 2026-10-30 04:39:53.731Z | 42.881° NE | 61.45° | 2026-10-30 04:43:53.731Z | 352.876° N |
| 6 mins | 2026-10-30 16:39:53.731Z | 57.082° ENE | 2026-10-30 16:42:53.731Z | 97.519° ESE | 21.106° | 2026-10-30 16:45:53.731Z | 135.091° SSE |
| 9 mins | 2026-10-30 18:16:53.731Z | 358.656° N | 2026-10-30 18:20:53.731Z | 287.61° WNW | 51.572° | 2026-10-30 18:25:53.731Z | 215.348° SW |
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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