FENGYUN 1C DEB, 29950
Orbit data source: Space-Track
FENGYUN 1C DEB, 29950 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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29950 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, 0.2 m
Radar Cross Section
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 FENGYUN 1C DEB
1 29950U 99025JY 26176.98353036 .00000083 00000-0 70327-4 0 9993
2 29950 98.7173 207.3890 0034017 51.1378 26.1721 14.10418066 438Epoch: 2026-06-25T23:36Z
TLE epoch observation values (Epoch: 2026-06-25T23:36:17.023Z)
Latitude
74.85012°
Longitude
-95.08591°
Altitude
848.63 km
Speed
7.446 km/s
True Right ascension
11h 32m 24s
True Declination
74° 45' 51"
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
20:39:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
879.719 km
Perigee altitude
830.508 km
Semi-major axis
7,233.25 km
Eccentricity
0.0034
Inclination
98.7173°
RAAN
207.389°
Arg. of periapsis
51.1378°
True anomaly
26.34469°
Mean anomaly
26.1721°
Eccentric anomaly
26.25833°
Mean motion
3.52812 °/min
Orbital period
102.04 mins
BSTAR
0.000070327
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-26 13:29:55.745Z | 69.81° E | 2026-06-26 13:31:55.745Z | 92.86° ESE | 13.274° | 2026-06-26 13:33:55.745Z | 115.178° SE |
| 9 mins | 2026-06-26 15:08:55.745Z | 8.122° NNE | 2026-06-26 15:12:55.745Z | 300.954° NW | 43.832° | 2026-06-26 15:17:55.745Z | 202.795° SW |
| 6 mins | 2026-06-27 00:56:55.745Z | 101.306° ESE | 2026-06-27 00:58:55.745Z | 72.104° E | 22.4° | 2026-06-27 01:02:55.745Z | 17.322° NNE |
| 9 mins | 2026-06-27 02:35:55.745Z | 195.613° SSW | 2026-06-27 02:39:55.745Z | 261.317° W | 34.046° | 2026-06-27 02:44:55.745Z | 331.912° NNW |
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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