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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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: 4 days ago
TLE from 4 days ago
0 FENGYUN 1C DEB *
1 46993U 99025EZT 26095.56847947 .00000390 00000-0 38855-3 0 9992
2 46993 98.7278 208.4417 0262280 358.2248 13.2486 13.69281748618156Epoch: 2026-04-05T13:38Z
TLE epoch observation values (Epoch: 2026-04-05T13:38:36.626Z)
Latitude
12.00024°
Longitude
168.05703°
Altitude
816.064 km
Speed
7.54 km/s
True Right ascension
13h 46m 19s
True Declination
11° 55' 52"
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
23:53:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,192.873 km
Perigee altitude
805.878 km
Semi-major axis
7,377.513 km
Eccentricity
0.02623
Inclination
98.7278°
RAAN
208.4417°
Arg. of periapsis
358.2248°
True anomaly
13.96005°
Mean anomaly
13.2486°
Eccentric anomaly
13.60201°
Mean motion
3.42514 °/min
Orbital period
105.11 mins
BSTAR
0.00038855
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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. |
|---|---|---|---|---|---|---|---|
| 13 mins | 2026-04-09 19:52:18.379Z | 22.328° NNE | 2026-04-09 19:59:18.379Z | 117.775° SE | 40.071° | 2026-04-09 20:05:18.379Z | 177.827° S |
| 9 mins | 2026-04-09 21:38:18.379Z | 340.091° N | 2026-04-09 21:42:18.379Z | 294.207° NW | 25.062° | 2026-04-09 21:47:18.379Z | 245.108° WSW |
| 5 mins | 2026-04-10 06:00:18.379Z | 85.421° E | 2026-04-10 06:02:18.379Z | 60.299° ENE | 17.278° | 2026-04-10 06:05:18.379Z | 25.787° NE |
| 10 mins | 2026-04-10 07:41:18.379Z | 179.982° S | 2026-04-10 07:45:18.379Z | 245.192° WSW | 41.806° | 2026-04-10 07:51:18.379Z | 340.472° 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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