FENGYUN 1C DEB, 31516
Orbit data source: Space-Track
FENGYUN 1C DEB, 31516 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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31516 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: 7 hours ago
TLE from 7 hours ago
0 FENGYUN 1C DEB
1 31516U 99025BXF 26169.60463220 .00000465 00000-0 19123-3 0 9992
2 31516 98.8522 292.0934 0148998 54.8548 323.6797 14.25801802991696Epoch: 2026-06-18T14:30Z
TLE epoch observation values (Epoch: 2026-06-18T14:30:40.222Z)
Latitude
17.28177°
Longitude
164.81791°
Altitude
722.422 km
Speed
7.54 km/s
True Right ascension
19h 17m 19s
True Declination
17° 11' 02"
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
07:53:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
909.952 km
Perigee altitude
695.958 km
Semi-major axis
7,181.092 km
Eccentricity
0.0149
Inclination
98.8522°
RAAN
292.0934°
Arg. of periapsis
54.8548°
True anomaly
322.65307°
Mean anomaly
323.6797°
Eccentric anomaly
323.16793°
Mean motion
3.56662 °/min
Orbital period
100.94 mins
BSTAR
0.00019123
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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 | 2026-06-18 21:43:56.454Z | 354.431° N | 2026-06-18 21:47:56.454Z | 285.325° WNW | 33.397° | 2026-06-18 21:51:56.454Z | 224.636° SW |
| 6 mins | 2026-06-19 07:25:56.454Z | 114.293° SE | 2026-06-19 07:27:56.454Z | 74.405° E | 28.123° | 2026-06-19 07:31:56.454Z | 8.306° NNE |
| 5 mins | 2026-06-19 09:05:56.454Z | 228.492° WSW | 2026-06-19 09:07:56.454Z | 263.224° W | 21.913° | 2026-06-19 09:10:56.454Z | 310.652° NW |
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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