FENGYUN 1C DEB, 30469
Orbit data source: Space-Track
FENGYUN 1C DEB, 30469 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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30469 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: 22 hours ago
TLE from 22 hours ago
0 FENGYUN 1C DEB
1 30469U 99025AGG 26066.54665873 .00001812 00000-0 11989-2 0 9993
2 30469 98.4762 275.6796 0158803 293.2297 93.1855 13.96786781968900Epoch: 2026-03-07T13:07Z
TLE epoch observation values (Epoch: 2026-03-07T13:07:11.314Z)
Latitude
27.93647°
Longitude
-90.89315°
Altitude
916.611 km
Speed
7.392 km/s
True Right ascension
18h 04m 40s
True Declination
27° 47' 51"
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
15:22:04
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,017.734 km
Perigee altitude
786.508 km
Semi-major axis
7,280.258 km
Eccentricity
0.01588
Inclination
98.4762°
RAAN
275.6796°
Arg. of periapsis
293.2297°
True anomaly
95.00013°
Mean anomaly
93.1855°
Eccentric anomaly
94.09305°
Mean motion
3.494 °/min
Orbital period
103.03 mins
BSTAR
0.0011989
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-03-08 13:10:50.035Z | 136.276° SSE | 2026-03-08 13:15:50.035Z | 58.966° ENE | 34.941° | 2026-03-08 13:20:50.035Z | 0.502° NNE |
| 8 mins | 2026-03-08 14:53:50.035Z | 219.188° SW | 2026-03-08 14:57:50.035Z | 272.828° WNW | 23.944° | 2026-03-08 15:01:50.035Z | 318.78° NNW |
| 8 mins | 2026-03-09 01:42:50.035Z | 46.242° ENE | 2026-03-09 01:46:50.035Z | 97.699° ESE | 25.322° | 2026-03-09 01:50:50.035Z | 145.51° SSE |
| 10 mins | 2026-03-09 03:23:50.035Z | 356.54° N | 2026-03-09 03:28:50.035Z | 282.605° WNW | 35.612° | 2026-03-09 03:33:50.035Z | 221.693° SW |
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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