FENGYUN 1C DEB, 30114
Orbit data source: Space-Track
FENGYUN 1C DEB, 30114 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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30114 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: 8 hours ago
TLE from 8 hours ago
0 FENGYUN 1C DEB
1 30114U 99025RT 26167.54975006 .00000167 00000-0 11634-3 0 9994
2 30114 98.7486 169.7552 0080232 315.0394 162.5873 14.09796454997723Epoch: 2026-06-16T13:11Z
TLE epoch observation values (Epoch: 2026-06-16T13:11:38.405Z)
Latitude
60.96084°
Longitude
-96.96946°
Altitude
925.902 km
Speed
7.366 km/s
True Right ascension
00h 23m 02s
True Declination
60° 49' 05"
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
07:36:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
915.293 km
Perigee altitude
799.191 km
Semi-major axis
7,235.379 km
Eccentricity
0.00802
Inclination
98.7486°
RAAN
169.7552°
Arg. of periapsis
315.0394°
True anomaly
162.85982°
Mean anomaly
162.5873°
Eccentric anomaly
162.72382°
Mean motion
3.52656 °/min
Orbital period
102.08 mins
BSTAR
0.00011634
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-16 23:00:23.319Z | 110.729° ESE | 2026-06-16 23:04:23.319Z | 56.598° ENE | 22.259° | 2026-06-16 23:07:23.319Z | 18.907° NNE |
| 9 mins | 2026-06-17 00:40:23.319Z | 193.447° SSW | 2026-06-17 00:44:23.319Z | 257.395° W | 35.259° | 2026-06-17 00:49:23.319Z | 331.988° NNW |
| 10 mins | 2026-06-17 13:04:23.319Z | 14.275° NNE | 2026-06-17 13:08:23.319Z | 24.151° NE | 44.679° | 2026-06-17 13:14:23.319Z | 194.619° SSW |
| 4 mins | 2026-06-17 14:47:23.319Z | 316.563° NNW | 2026-06-17 14:48:23.319Z | 305.454° NW | 13.771° | 2026-06-17 14:51:23.319Z | 273.395° WNW |
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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