FENGYUN 1C DEB, 40688
Orbit data source: Space-Track
FENGYUN 1C DEB, 40688 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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40688 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, 0.050 m
Radar Cross Section
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 2 weeks ago
TLE from 2 weeks ago
0 FENGYUN 1C DEB
1 40688U 99025EWU 26273.59535757 .00000245 00000-0 24001-3 0 9998
2 40688 99.0066 55.5237 0141040 325.9154 33.3004 13.84080848339545Epoch: 2026-09-30T14:17Z
TLE epoch observation values (Epoch: 2026-09-30T14:17:18.894Z)
Latitude
-0.00002°
Longitude
-168.14878°
Altitude
866.357 km
Speed
7.463 km/s
True Right ascension
03h 42m 05s
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
00:12:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,049.977 km
Perigee altitude
843.359 km
Semi-major axis
7,324.805 km
Eccentricity
0.0141
Inclination
99.0066°
RAAN
55.5237°
Arg. of periapsis
325.9154°
True anomaly
34.20097°
Mean anomaly
33.3004°
Eccentric anomaly
33.74935°
Mean motion
3.46218 °/min
Orbital period
103.98 mins
BSTAR
0.00024001
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-10-11 08:54:21.767Z | 140.803° SSE | 2026-10-11 08:59:21.767Z | 79.457° E | 48.584° | 2026-10-11 09:05:21.767Z | 357.76° N |
| 8 mins | 2026-10-11 10:39:21.767Z | 224.728° SW | 2026-10-11 10:42:21.767Z | 262.891° W | 24.984° | 2026-10-11 10:47:21.767Z | 319.184° NNW |
| 9 mins | 2026-10-11 21:33:21.767Z | 41.08° NE | 2026-10-11 21:37:21.767Z | 90.352° ESE | 33.253° | 2026-10-11 21:42:21.767Z | 153.467° SSE |
| 10 mins | 2026-10-11 23:15:21.767Z | 355.743° N | 2026-10-11 23:20:21.767Z | 291.979° WNW | 41.357° | 2026-10-11 23:25:21.767Z | 228.627° WSW |
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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