FENGYUN 1C DEB, 30342
Orbit data source: Space-Track
FENGYUN 1C DEB, 30342 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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30342 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: 6 hours ago
TLE from 6 hours ago
0 FENGYUN 1C DEB
1 30342U 99025ABD 26059.13030615 .00000574 00000-0 54166-3 0 9999
2 30342 100.2000 249.6177 0167529 283.7678 195.6214 13.80155397959568Epoch: 2026-02-28T03:07Z
TLE epoch observation values (Epoch: 2026-02-28T03:07:38.451Z)
Latitude
59.61091°
Longitude
-117.47632°
Altitude
1,091.975 km
Speed
7.252 km/s
True Right ascension
05h 49m 33s
True Declination
59° 28' 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
12:30:19
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,083.568 km
Perigee altitude
837.677 km
Semi-major axis
7,338.759 km
Eccentricity
0.01675
Inclination
100.2°
RAAN
249.6177°
Arg. of periapsis
283.7678°
True anomaly
195.11469°
Mean anomaly
195.6214°
Eccentric anomaly
195.36703°
Mean motion
3.45231 °/min
Orbital period
104.28 mins
BSTAR
0.00054166
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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 | 2026-02-28 11:23:00.867Z | 116.77° SE | 2026-02-28 11:28:00.867Z | 56.545° ENE | 26.392° | 2026-02-28 11:33:00.867Z | 5.165° NNE |
| 10 mins | 2026-02-28 13:06:00.867Z | 194.574° SSW | 2026-02-28 13:10:00.867Z | 255.074° W | 35.918° | 2026-02-28 13:16:00.867Z | 331.662° NNW |
| 6 mins | 2026-03-01 00:05:00.867Z | 67.772° E | 2026-03-01 00:07:00.867Z | 88.499° E | 16.016° | 2026-03-01 00:11:00.867Z | 127.917° SE |
| 11 mins | 2026-03-01 01:46:00.867Z | 11.379° NNE | 2026-03-01 01:51:00.867Z | 253.256° W | 44.188° | 2026-03-01 01:57:00.867Z | 202.767° SW |
| 4 mins | 2026-03-01 03:31:00.867Z | 319.975° NNW | 2026-03-01 03:32:00.867Z | 310.077° NW | 14.062° | 2026-03-01 03:35:00.867Z | 280.969° WNW |
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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