FENGYUN 1C DEB *, 49389
Orbit data source: Space-Track
FENGYUN 1C DEB *, 49389 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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49389 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: 1 month ago
TLE from 1 month ago
0 FENGYUN 1C DEB *
1 49389U 99025FCJ 26070.24001725 .00003391 00000-0 21372-2 0 9997
2 49389 98.7028 261.6924 0135810 303.6751 55.1524 14.00437005240879Epoch: 2026-03-11T05:45Z
TLE epoch observation values (Epoch: 2026-03-11T05:45:37.490Z)
Latitude
-0.00005°
Longitude
6.3791°
Altitude
839.655 km
Speed
7.461 km/s
True Right ascension
17h 26m 46s
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
19:11:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
988.167 km
Perigee altitude
790.765 km
Semi-major axis
7,267.603 km
Eccentricity
0.01358
Inclination
98.7028°
RAAN
261.6924°
Arg. of periapsis
303.6751°
True anomaly
56.44199°
Mean anomaly
55.1524°
Eccentric anomaly
55.79595°
Mean motion
3.50313 °/min
Orbital period
102.77 mins
BSTAR
0.0021372
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-04-22 12:52:11.506Z | 180.092° SSW | 2026-04-22 12:57:11.506Z | 251.545° W | 41.475° | 2026-04-22 13:03:11.506Z | 339.364° N |
| 9 mins | 2026-04-23 01:22:11.506Z | 19.161° NNE | 2026-04-23 01:26:11.506Z | 114.954° SE | 43.967° | 2026-04-23 01:31:11.506Z | 188.406° SSW |
| 4 mins | 2026-04-23 03:05:11.506Z | 321.331° NNW | 2026-04-23 03:07:11.506Z | 297.147° NW | 13.944° | 2026-04-23 03:09:11.506Z | 273.737° WNW |
| 7 mins | 2026-04-23 11:13:11.506Z | 100.023° ESE | 2026-04-23 11:16:11.506Z | 65.152° ENE | 20.063° | 2026-04-23 11:20:11.506Z | 19.612° NNE |
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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