FENGYUN 1C DEB, 30193
Orbit data source: Space-Track
FENGYUN 1C DEB, 30193 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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30193 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: 16 hours ago
TLE from 16 hours ago
0 FENGYUN 1C DEB
1 30193U 99025VA 26059.32053642 .00003389 00000-0 83229-3 0 9998
2 30193 98.7555 335.4937 0104195 259.7807 221.4828 14.49813933 2913Epoch: 2026-02-28T07:41Z
TLE epoch observation values (Epoch: 2026-02-28T07:41:34.346Z)
Latitude
58.50243°
Longitude
-103.56525°
Altitude
791.915 km
Speed
7.434 km/s
True Right ascension
11h 19m 53s
True Declination
58° 20' 59"
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
03:26:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
797.371 km
Perigee altitude
649.383 km
Semi-major axis
7,101.514 km
Eccentricity
0.01042
Inclination
98.7555°
RAAN
335.4937°
Arg. of periapsis
259.7807°
True anomaly
220.69958°
Mean anomaly
221.4828°
Eccentric anomaly
221.09043°
Mean motion
3.62674 °/min
Orbital period
99.26 mins
BSTAR
0.00083229
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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 | 2026-03-01 06:54:04.918Z | 24.095° NE | 2026-03-01 06:58:04.918Z | 81.166° E | 39.142° | 2026-03-01 07:03:04.918Z | 178.649° S |
| 5 mins | 2026-03-01 08:34:04.918Z | 325.777° NNW | 2026-03-01 08:36:04.918Z | 298.342° NW | 17.045° | 2026-03-01 08:39:04.918Z | 259.502° W |
| 8 mins | 2026-03-01 18:03:04.918Z | 149.875° SSE | 2026-03-01 18:06:04.918Z | 87.81° E | 42.406° | 2026-03-01 18:11:04.918Z | 352.7° N |
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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