FENGYUN 1C DEB, 30673
Orbit data source: Space-Track
FENGYUN 1C DEB, 30673 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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30673 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, 0.095 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 FENGYUN 1C DEB
1 30673U 99025AQF 26279.39307266 -.00000104 00000-0 -38651-4 0 9990
2 30673 98.8796 327.1470 0052345 34.6152 336.4986 14.03586993 7073Epoch: 2026-10-06T09:26Z
TLE epoch observation values (Epoch: 2026-10-06T09:26:01.477Z)
Latitude
10.69141°
Longitude
168.90129°
Altitude
848.712 km
Speed
7.447 km/s
True Right ascension
21h 41m 51s
True Declination
10° 37' 47"
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
14:56:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
916.574 km
Perigee altitude
840.604 km
Semi-major axis
7,256.726 km
Eccentricity
0.00523
Inclination
98.8796°
RAAN
327.147°
Arg. of periapsis
34.6152°
True anomaly
336.25796°
Mean anomaly
336.4986°
Eccentric anomaly
336.37843°
Mean motion
3.51101 °/min
Orbital period
102.53 mins
BSTAR
-0.000038651
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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 | 2026-10-07 02:36:55.134Z | 136.358° SSE | 2026-10-07 02:41:55.134Z | 56.561° ENE | 41.495° | 2026-10-07 02:45:55.134Z | 3.078° NNE |
| 7 mins | 2026-10-07 04:19:55.134Z | 223.121° SW | 2026-10-07 04:22:55.134Z | 265.164° W | 24.147° | 2026-10-07 04:26:55.134Z | 316.085° NNW |
| 7 mins | 2026-10-07 15:04:55.134Z | 52.105° ENE | 2026-10-07 15:07:55.134Z | 89.642° E | 22.38° | 2026-10-07 15:11:55.134Z | 139.149° SSE |
| 9 mins | 2026-10-07 16:45:55.134Z | 356.156° N | 2026-10-07 16:49:55.134Z | 282.34° WNW | 49.331° | 2026-10-07 16:54:55.134Z | 217.166° 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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