FENGYUN 1C DEB, 30516
Orbit data source: Space-Track
FENGYUN 1C DEB, 30516 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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30516 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 FENGYUN 1C DEB
1 30516U 99025AJE 26255.29594907 .00003638 00000-0 10578-2 0 9998
2 30516 98.8655 15.2189 0009676 192.7940 196.7468 14.44885217 16613Epoch: 2026-09-12T07:06Z
TLE epoch observation values (Epoch: 2026-09-12T07:06:09.999Z)
Latitude
29.1711°
Longitude
-87.59811°
Altitude
752.64 km
Speed
7.477 km/s
True Right ascension
00h 41m 00s
True Declination
29° 01' 30"
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
09:43:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
746.423 km
Perigee altitude
732.649 km
Semi-major axis
7,117.673 km
Eccentricity
0.00097
Inclination
98.8655°
RAAN
15.2189°
Arg. of periapsis
192.794°
True anomaly
196.71489°
Mean anomaly
196.7468°
Eccentric anomaly
196.73084°
Mean motion
3.6144 °/min
Orbital period
99.6 mins
BSTAR
0.0010578
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-09-12 20:49:41.532Z | 18.577° NNE | 2026-09-12 20:54:41.532Z | 114.327° SE | 69.504° | 2026-09-12 20:58:41.532Z | 185.265° SSW |
| 8 mins | 2026-09-13 08:01:41.532Z | 163.397° S | 2026-09-13 08:04:41.532Z | 150.664° SSE | 79.239° | 2026-09-13 08:09:41.532Z | 347.008° N |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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