FENGYUN 1C DEB, 39536
Orbit data source: Space-Track
FENGYUN 1C DEB, 39536 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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39536 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: 1 month ago
TLE from 1 month ago
0 FENGYUN 1C DEB
1 39536U 99025EWD 26195.34948763 .00000475 00000-0 47907-3 0 9994
2 39536 99.7733 243.9331 0241692 69.5215 293.1697 13.70343794646894Epoch: 2026-07-14T08:23Z
TLE epoch observation values (Epoch: 2026-07-14T08:23:15.731Z)
Latitude
-0.00001°
Longitude
-174.10336°
Altitude
934.683 km
Speed
7.418 km/s
True Right ascension
16h 15m 43s
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
06:22:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,173.83 km
Perigee altitude
817.395 km
Semi-major axis
7,373.75 km
Eccentricity
0.02417
Inclination
99.7733°
RAAN
243.9331°
Arg. of periapsis
69.5215°
True anomaly
290.59375°
Mean anomaly
293.1697°
Eccentric anomaly
291.8847°
Mean motion
3.42776 °/min
Orbital period
105.02 mins
BSTAR
0.00047907
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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 | 2026-08-26 16:02:28.031Z | 19.872° NNE | 2026-08-26 16:09:28.031Z | 122.746° SE | 43.119° | 2026-08-26 16:15:28.031Z | 186.162° SSW |
| 8 mins | 2026-08-26 17:48:28.031Z | 338.205° N | 2026-08-26 17:52:28.031Z | 295.077° NW | 22.022° | 2026-08-26 17:56:28.031Z | 256.419° W |
| 8 mins | 2026-08-27 02:08:28.031Z | 103.061° ESE | 2026-08-27 02:11:28.031Z | 62.282° ENE | 24.634° | 2026-08-27 02:16:28.031Z | 7.939° NNE |
| 10 mins | 2026-08-27 03:50:28.031Z | 192.452° SSW | 2026-08-27 03:54:28.031Z | 251.727° W | 36.164° | 2026-08-27 04:00:28.031Z | 332.835° NNW |
| 9 mins | 2026-08-27 14:52:28.031Z | 52.79° ENE | 2026-08-27 14:56:28.031Z | 91.661° ESE | 19.619° | 2026-08-27 15:01:28.031Z | 137.675° SSE |
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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