FENGYUN 1C DEB, 30360
Orbit data source: Space-Track
FENGYUN 1C DEB, 30360 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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30360 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: 1 week ago
TLE from 1 week ago
0 FENGYUN 1C DEB
1 30360U 99025ABX 26153.18200603 .00003003 00000-0 12314-2 0 9993
2 30360 98.7506 227.9771 0028126 12.4437 42.7588 14.27652896998701Epoch: 2026-06-02T04:22Z
TLE epoch observation values (Epoch: 2026-06-02T04:22:05.320Z)
Latitude
54.56699°
Longitude
-100.6298°
Altitude
793.763 km
Speed
7.47 km/s
True Right ascension
14h 22m 12s
True Declination
54° 24' 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
02:41:01
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
816.917 km
Perigee altitude
776.557 km
Semi-major axis
7,174.874 km
Eccentricity
0.00281
Inclination
98.7506°
RAAN
227.9771°
Arg. of periapsis
12.4437°
True anomaly
42.97818°
Mean anomaly
42.7588°
Eccentric anomaly
42.86843°
Mean motion
3.57126 °/min
Orbital period
100.8 mins
BSTAR
0.0012314
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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 | 2026-06-10 17:53:20.270Z | 14.47° NNE | 2026-06-10 17:58:20.270Z | 179.458° S | 44.391° | 2026-06-10 18:02:20.270Z | 193.539° SSW |
| 4 mins | 2026-06-11 03:35:20.270Z | 86.964° E | 2026-06-11 03:37:20.270Z | 61.019° ENE | 15.47° | 2026-06-11 03:39:20.270Z | 35.318° NE |
| 9 mins | 2026-06-11 05:12:20.270Z | 178.598° S | 2026-06-11 05:16:20.270Z | 254.236° W | 42.093° | 2026-06-11 05:21:20.270Z | 339.846° N |
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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