FENGYUN 1C DEB, 47027
Orbit data source: Space-Track
FENGYUN 1C DEB, 47027 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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47027 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
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 47027U 99025FBD 26313.42007164 .00011645 00000-0 30016-2 0 9993
2 47027 98.4918 7.9076 0058989 354.5522 17.9606 14.49154848746751Epoch: 2026-11-09T10:04Z
TLE epoch observation values (Epoch: 2026-11-09T10:04:54.189Z)
Latitude
12.5412°
Longitude
166.1919°
Altitude
690.751 km
Speed
7.533 km/s
True Right ascension
00h 24m 03s
True Declination
12° 28' 04"
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
18:12:27
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
767.423 km
Perigee altitude
683.616 km
Semi-major axis
7,103.656 km
Eccentricity
0.0059
Inclination
98.4918°
RAAN
7.9076°
Arg. of periapsis
354.5522°
True anomaly
18.17051°
Mean anomaly
17.9606°
Eccentric anomaly
18.06541°
Mean motion
3.6251 °/min
Orbital period
99.31 mins
BSTAR
0.0030016
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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 | 2026-11-11 03:33:39.598Z | 156.735° SSE | 2026-11-11 03:38:39.598Z | 36.347° NE | 65.013° | 2026-11-11 03:42:39.598Z | 352.08° N |
| 6 mins | 2026-11-11 15:39:39.598Z | 58.262° ENE | 2026-11-11 15:41:39.598Z | 87.364° E | 21.544° | 2026-11-11 15:45:39.598Z | 141.751° SSE |
| 8 mins | 2026-11-11 17:16:39.598Z | 354.415° N | 2026-11-11 17:20:39.598Z | 281.141° WNW | 42.331° | 2026-11-11 17:24:39.598Z | 221.86° SW |
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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