FENGYUN 1C DEB, 30694
Orbit data source: Space-Track
FENGYUN 1C DEB, 30694 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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30694 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: 10 hours ago
TLE from 10 hours ago
0 FENGYUN 1C DEB
1 30694U 99025ARC 26109.93433258 .00005216 00000-0 48053-3 0 9999
2 30694 99.0598 99.2316 0123505 246.0605 112.7633 14.89602318 20022Epoch: 2026-04-19T22:25Z
TLE epoch observation values (Epoch: 2026-04-19T22:25:26.334Z)
Latitude
-0.0001°
Longitude
-85.15981°
Altitude
636.423 km
Speed
7.521 km/s
True Right ascension
06h 36m 55s
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
14:54:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
682.398 km
Perigee altitude
510.123 km
Semi-major axis
6,974.397 km
Eccentricity
0.01235
Inclination
99.0598°
RAAN
99.2316°
Arg. of periapsis
246.0605°
True anomaly
114.06047°
Mean anomaly
112.7633°
Eccentric anomaly
113.41267°
Mean motion
3.72635 °/min
Orbital period
96.61 mins
BSTAR
0.00048053
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-04-20 11:53:48.783Z | 24.689° NE | 2026-04-20 11:57:48.783Z | 112.283° ESE | 39.068° | 2026-04-20 12:00:48.783Z | 176.031° S |
| 7 mins | 2026-04-20 22:44:48.783Z | 136.023° SSE | 2026-04-20 22:47:48.783Z | 71.483° E | 35.73° | 2026-04-20 22:51:48.783Z | 0.309° NNE |
| 4 mins | 2026-04-21 00:21:48.783Z | 239.433° WSW | 2026-04-21 00:23:48.783Z | 270.351° WNW | 16.617° | 2026-04-21 00:25:48.783Z | 299.193° 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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