FENGYUN 1C DEB, 38824
Orbit data source: Space-Track
FENGYUN 1C DEB, 38824 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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38824 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 38824U 99025EVQ 26105.84511537 .00003028 00000-0 14993-2 0 9999
2 38824 99.2950 249.5717 0096714 212.4621 147.0580 14.15676249708927Epoch: 2026-04-15T20:16Z
TLE epoch observation values (Epoch: 2026-04-15T20:16:57.967Z)
Latitude
-0.00002°
Longitude
101.329°
Altitude
901.696 km
Speed
7.371 km/s
True Right ascension
16h 38m 17s
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
14:54:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
906.988 km
Perigee altitude
767.423 km
Semi-major axis
7,215.342 km
Eccentricity
0.00967
Inclination
99.295°
RAAN
249.5717°
Arg. of periapsis
212.4621°
True anomaly
147.65459°
Mean anomaly
147.058°
Eccentric anomaly
147.3569°
Mean motion
3.54126 °/min
Orbital period
101.66 mins
BSTAR
0.0014993
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-04-20 08:57:17.436Z | 143.617° SSE | 2026-04-20 09:02:17.436Z | 83.445° E | 37.603° | 2026-04-20 09:07:17.436Z | 358.995° N |
| 7 mins | 2026-04-20 10:40:17.436Z | 227.215° WSW | 2026-04-20 10:43:17.436Z | 266.035° W | 20.954° | 2026-04-20 10:47:17.436Z | 313.353° NW |
| 5 mins | 2026-04-20 21:21:17.436Z | 65.19° ENE | 2026-04-20 21:23:17.436Z | 93.308° ESE | 18.316° | 2026-04-20 21:26:17.436Z | 132.725° SE |
| 8 mins | 2026-04-20 23:00:17.436Z | 357.817° N | 2026-04-20 23:04:17.436Z | 278.397° WNW | 36.881° | 2026-04-20 23:08:17.436Z | 218.723° SW |
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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