FENGYUN 1C DEB, 30037
Orbit data source: Space-Track
FENGYUN 1C DEB, 30037 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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30037 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: 16 hours ago
TLE from 16 hours ago
0 FENGYUN 1C DEB
1 30037U 99025NN 26255.15490832 .00000334 00000-0 11529-3 0 9991
2 30037 98.4158 228.3625 0172071 321.2745 95.6537 14.34429223 27075Epoch: 2026-09-12T03:43Z
TLE epoch observation values (Epoch: 2026-09-12T03:43:04.078Z)
Latitude
57.97699°
Longitude
167.81817°
Altitude
800.937 km
Speed
7.451 km/s
True Right ascension
14h 19m 00s
True Declination
57° 49' 23"
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
11:41:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
897.157 km
Perigee altitude
651.019 km
Semi-major axis
7,152.225 km
Eccentricity
0.01721
Inclination
98.4158°
RAAN
228.3625°
Arg. of periapsis
321.2745°
True anomaly
97.61137°
Mean anomaly
95.6537°
Eccentric anomaly
96.633°
Mean motion
3.58824 °/min
Orbital period
100.33 mins
BSTAR
0.00011529
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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 | 2026-09-12 21:59:09.310Z | 149.736° SSE | 2026-09-12 22:03:09.310Z | 67.377° ENE | 60.832° | 2026-09-12 22:08:09.310Z | 354.035° N |
| 8 mins | 2026-09-13 10:11:09.310Z | 46.752° ENE | 2026-09-13 10:15:09.310Z | 100.931° ESE | 26.061° | 2026-09-13 10:19:09.310Z | 147.692° SSE |
| 9 mins | 2026-09-13 11:50:09.310Z | 353.365° N | 2026-09-13 11:54:09.310Z | 287.026° WNW | 44.609° | 2026-09-13 11:59:09.310Z | 220.817° 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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