FENGYUN 1C DEB, 36676
Orbit data source: Space-Track
FENGYUN 1C DEB, 36676 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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36676 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: 14 hours ago
TLE from 14 hours ago
0 FENGYUN 1C DEB
1 36676U 99025DYW 26207.58828883 .00001017 00000-0 29681-3 0 9998
2 36676 98.7556 118.6644 0093956 176.0591 306.5588 14.43858994683244Epoch: 2026-07-26T14:07Z
TLE epoch observation values (Epoch: 2026-07-26T14:07:08.154Z)
Latitude
57.29081°
Longitude
156.39613°
Altitude
715.9 km
Speed
7.524 km/s
True Right ascension
20h 49m 51s
True Declination
57° 07' 60"
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
17:04:35
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
809.812 km
Perigee altitude
675.999 km
Semi-major axis
7,121.042 km
Eccentricity
0.0094
Inclination
98.7556°
RAAN
118.6644°
Arg. of periapsis
176.0591°
True anomaly
305.68792°
Mean anomaly
306.5588°
Eccentric anomaly
306.12397°
Mean motion
3.61183 °/min
Orbital period
99.67 mins
BSTAR
0.00029681
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-07-27 06:45:41.463Z | 22.044° NNE | 2026-07-27 06:49:41.463Z | 77.215° E | 39.812° | 2026-07-27 06:53:41.463Z | 178.35° S |
| 8 mins | 2026-07-27 17:57:41.463Z | 157.464° SSE | 2026-07-27 18:00:41.463Z | 122.414° SE | 43.467° | 2026-07-27 18:05:41.463Z | 349.956° 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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