FENGYUN 1C DEB, 30550
Orbit data source: Space-Track
FENGYUN 1C DEB, 30550 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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30550 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: 2 days ago
TLE from 2 days ago
0 FENGYUN 1C DEB
1 30550U 99025AKQ 26261.23605656 .00001643 00000-0 99395-3 0 9990
2 30550 99.0440 160.2029 0125101 241.9572 271.9297 14.04132660993152Epoch: 2026-09-18T05:39Z
TLE epoch observation values (Epoch: 2026-09-18T05:39:55.286Z)
Latitude
27.21511°
Longitude
-97.26878°
Altitude
880.892 km
Speed
7.415 km/s
True Right ascension
22h 59m 29s
True Declination
27° 04' 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
12:10:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
967.474 km
Perigee altitude
785.956 km
Semi-major axis
7,254.852 km
Eccentricity
0.01251
Inclination
99.044°
RAAN
160.2029°
Arg. of periapsis
241.9572°
True anomaly
270.49636°
Mean anomaly
271.9297°
Eccentric anomaly
271.21308°
Mean motion
3.51237 °/min
Orbital period
102.49 mins
BSTAR
0.00099395
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-09-20 05:24:59.321Z | 35.397° NE | 2026-09-20 05:29:59.321Z | 98.584° ESE | 31.241° | 2026-09-20 05:33:59.321Z | 152.839° SSE |
| 9 mins | 2026-09-20 07:06:59.321Z | 351.344° N | 2026-09-20 07:10:59.321Z | 295.347° NW | 35.924° | 2026-09-20 07:15:59.321Z | 229.48° WSW |
| 10 mins | 2026-09-20 16:54:59.321Z | 144.852° SSE | 2026-09-20 16:58:59.321Z | 82.024° E | 59.448° | 2026-09-20 17:04:59.321Z | 354.093° N |
| 7 mins | 2026-09-20 18:37:59.321Z | 233.768° WSW | 2026-09-20 18:40:59.321Z | 270.128° WNW | 20.758° | 2026-09-20 18:44:59.321Z | 312.857° NW |
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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