FENGYUN 1C DEB, 30115
Orbit data source: Space-Track
FENGYUN 1C DEB, 30115 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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30115 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 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 30115U 99025RU 26236.01941878 .00001299 00000-0 60804-3 0 9994
2 30115 98.6035 261.6263 0067488 46.2615 334.7602 14.20699267 9387Epoch: 2026-08-24T00:27Z
TLE epoch observation values (Epoch: 2026-08-24T00:27:57.782Z)
Latitude
20.45244°
Longitude
-80.88896°
Altitude
781.624 km
Speed
7.488 km/s
True Right ascension
17h 13m 38s
True Declination
20° 20' 26"
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
18:20:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
868.721 km
Perigee altitude
771.562 km
Semi-major axis
7,198.278 km
Eccentricity
0.00675
Inclination
98.6035°
RAAN
261.6263°
Arg. of periapsis
46.2615°
True anomaly
334.4279°
Mean anomaly
334.7602°
Eccentric anomaly
334.59431°
Mean motion
3.55386 °/min
Orbital period
101.3 mins
BSTAR
0.00060804
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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 | 2026-08-25 14:07:38.272Z | 27.222° NE | 2026-08-25 14:12:38.272Z | 98.459° ESE | 34.816° | 2026-08-25 14:17:38.272Z | 170.254° S |
| 7 mins | 2026-08-25 15:49:38.272Z | 335.775° NNW | 2026-08-25 15:52:38.272Z | 292.732° NW | 22.004° | 2026-08-25 15:56:38.272Z | 243.828° WSW |
| 8 mins | 2026-08-26 01:31:38.272Z | 150.076° SSE | 2026-08-26 01:34:38.272Z | 77.811° E | 42.612° | 2026-08-26 01:39:38.272Z | 352.447° 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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