FENGYUN 1C DEB *, 47015
Orbit data source: Space-Track
FENGYUN 1C DEB *, 47015 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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47015 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: 2 days ago
TLE from 2 days ago
0 FENGYUN 1C DEB *
1 47015U 99025FAR 26084.15582815 .00010217 00000-0 82532-3 0 9991
2 47015 98.6913 155.8775 0170505 142.9435 218.3699 14.89284947659058Epoch: 2026-03-25T03:44Z
TLE epoch observation values (Epoch: 2026-03-25T03:44:23.552Z)
Latitude
0.00007°
Longitude
-82.84383°
Altitude
697.251 km
Speed
7.457 km/s
True Right ascension
10h 23m 30s
True Declination
0° 00' 00"
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
23:24:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
716.166 km
Perigee altitude
478.299 km
Semi-major axis
6,975.37 km
Eccentricity
0.01705
Inclination
98.6913°
RAAN
155.8775°
Arg. of periapsis
142.9435°
True anomaly
217.17711°
Mean anomaly
218.3699°
Eccentric anomaly
217.77152°
Mean motion
3.72557 °/min
Orbital period
96.63 mins
BSTAR
0.00082532
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-27 04:14:16.852Z | 142.731° SSE | 2026-03-27 04:18:16.852Z | 70.353° E | 34.612° | 2026-03-27 04:21:16.852Z | 5.327° NNE |
| 5 mins | 2026-03-27 17:36:16.852Z | 22.735° NE | 2026-03-27 17:38:16.852Z | 151.537° SSE | 42.62° | 2026-03-27 17:41:16.852Z | 188.734° SSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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