FENGYUN 1C DEB *, 46993
Orbit data source: Space-Track
FENGYUN 1C DEB *, 46993 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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46993 intel report (Beta)
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Edit Public Description
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
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 5 days ago
TLE from 5 days ago
0 FENGYUN 1C DEB *
1 46993U 99025EZT 25252.60439910 .00000377 00000-0 37615-3 0 9996
2 46993 98.7144 19.8806 0264638 188.4803 238.8150 13.69045159589696Epoch: 2025-09-09T14:30Z
TLE epoch observation values (Epoch: 2025-09-09T14:30:20.082Z)
Latitude
63.46585°
Longitude
155.62145°
Altitude
1,118.742 km
Speed
7.247 km/s
True Right ascension
00h 08m 23s
True Declination
63° 20' 05"
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
21:24:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,195.485 km
Perigee altitude
804.966 km
Semi-major axis
7,378.362 km
Eccentricity
0.02646
Inclination
98.7144°
RAAN
19.8806°
Arg. of periapsis
188.4803°
True anomaly
236.26523°
Mean anomaly
238.815°
Eccentric anomaly
237.53569°
Mean motion
3.42455 °/min
Orbital period
105.12 mins
BSTAR
0.00037615
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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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2025-09-14 06:38:25.454Z | 80.722° E | 2025-09-14 06:41:25.454Z | 52.962° ENE | 13.913° | 2025-09-14 06:43:25.454Z | 34.349° NE |
| 12 mins | 2025-09-14 08:18:25.454Z | 157.49° SSE | 2025-09-14 08:23:25.454Z | 110.098° ESE | 44.062° | 2025-09-14 08:30:25.454Z | 349.529° N |
| 7 mins | 2025-09-14 10:05:25.454Z | 242.401° WSW | 2025-09-14 10:08:25.454Z | 272.484° WNW | 17.375° | 2025-09-14 10:12:25.454Z | 309.462° NW |
| 9 mins | 2025-09-14 21:05:25.454Z | 26.372° NE | 2025-09-14 21:09:25.454Z | 100.218° ESE | 39.855° | 2025-09-14 21:14:25.454Z | 178.548° S |
| 5 mins | 2025-09-14 22:50:25.454Z | 328.868° NNW | 2025-09-14 22:52:25.454Z | 303.839° NW | 17.588° | 2025-09-14 22:55:25.454Z | 265.089° W |
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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