FENGYUN 1C DEB, 30194 (Decayed)
Orbit data source: Space-Track
FENGYUN 1C DEB, 30194 was 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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30194 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
Unknown
Mission
Decayed 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: 6 months ago
TLE from 6 months ago
0 FENGYUN 1C DEB
1 30194U 99025VB 25102.30903696 .05311450 47404-1 26788-1 0 9999
2 30194 101.1836 313.3459 0011368 277.8101 82.1866 15.87790495951890Epoch: 2025-04-12T07:25Z
TLE epoch observation values (Epoch: 2025-04-12T07:25:00.793Z)
Latitude
-0.00003°
Longitude
1.33805°
Altitude
310.497 km
Speed
7.722 km/s
True Right ascension
20h 53m 23s
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
17:49:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
313.16 km
Perigee altitude
297.964 km
Semi-major axis
6,683.699 km
Eccentricity
0.00114
Inclination
101.1836°
RAAN
313.3459°
Arg. of periapsis
277.8101°
True anomaly
82.31568°
Mean anomaly
82.1866°
Eccentric anomaly
82.25114°
Mean motion
3.97208 °/min
Orbital period
90.63 mins
BSTAR
0.026788
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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
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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. |
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| This satellite is decayed. |
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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