FENGYUN 1C DEB, 30567
Orbit data source: Space-Track
FENGYUN 1C DEB, 30567 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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30567 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
Medium (>0.1 m² and <1 m²)
Expand to show TLE details & historyLast TLE update: 1 week ago
TLE from 1 week ago
0 FENGYUN 1C DEB
1 30567U 99025ALH 26154.68938201 .00000610 00000-0 35553-3 0 9992
2 30567 98.7875 146.0337 0110069 61.7521 354.3495 14.09089989992099Epoch: 2026-06-03T16:32Z
TLE epoch observation values (Epoch: 2026-06-03T16:32:42.605Z)
Latitude
55.09319°
Longitude
-7.01812°
Altitude
792.256 km
Speed
7.504 km/s
True Right ascension
08h 53m 12s
True Declination
54° 55' 57"
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
02:42:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
939.33 km
Perigee altitude
779.998 km
Semi-major axis
7,237.801 km
Eccentricity
0.01101
Inclination
98.7875°
RAAN
146.0337°
Arg. of periapsis
61.7521°
True anomaly
354.22359°
Mean anomaly
354.3495°
Eccentric anomaly
354.28672°
Mean motion
3.52479 °/min
Orbital period
102.13 mins
BSTAR
0.00035553
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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 | 2026-06-10 22:15:30.968Z | 110.952° ESE | 2026-06-10 22:19:30.968Z | 56.016° ENE | 20.367° | 2026-06-10 22:22:30.968Z | 18.115° NNE |
| 8 mins | 2026-06-10 23:56:30.968Z | 199.048° SSW | 2026-06-10 23:59:30.968Z | 255.487° W | 34.183° | 2026-06-11 00:04:30.968Z | 332.298° NNW |
| 9 mins | 2026-06-11 12:19:30.968Z | 14.802° NNE | 2026-06-11 12:23:30.968Z | 66.481° ENE | 44.947° | 2026-06-11 12:28:30.968Z | 193.877° SSW |
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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