FENGYUN 1C DEB, 30390
Orbit data source: Space-Track
FENGYUN 1C DEB, 30390 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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30390 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, 0.050 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 FENGYUN 1C DEB
1 30390U 99025ADD 26296.24993752 .00002751 00000-0 10207-2 0 9993
2 30390 98.8155 28.9749 0063787 324.7691 59.9057 14.31912129 18822Epoch: 2026-10-23T05:59Z
TLE epoch observation values (Epoch: 2026-10-23T05:59:54.601Z)
Latitude
25.01993°
Longitude
-96.80447°
Altitude
765.686 km
Speed
7.485 km/s
True Right ascension
01h 39m 23s
True Declination
24° 53' 19"
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
21:44:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
828.17 km
Perigee altitude
736.819 km
Semi-major axis
7,160.631 km
Eccentricity
0.00638
Inclination
98.8155°
RAAN
28.9749°
Arg. of periapsis
324.7691°
True anomaly
60.54064°
Mean anomaly
59.9057°
Eccentric anomaly
60.22292°
Mean motion
3.58192 °/min
Orbital period
100.5 mins
BSTAR
0.0010207
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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 | 2026-10-24 05:29:16.725Z | 129.346° SE | 2026-10-24 05:33:16.725Z | 75.486° E | 32.912° | 2026-10-24 05:37:16.725Z | 10.719° NNE |
| 7 mins | 2026-10-24 07:10:16.725Z | 219.459° SW | 2026-10-24 07:13:16.725Z | 271.149° WNW | 27.988° | 2026-10-24 07:17:16.725Z | 322.608° NNW |
| 9 mins | 2026-10-24 19:21:16.725Z | 10.6° NNE | 2026-10-24 19:25:16.725Z | 332.243° NNW | 75.818° | 2026-10-24 19:30:16.725Z | 199.97° SSW |
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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