FENGYUN 1C DEB, 30069
Orbit data source: Space-Track
FENGYUN 1C DEB, 30069 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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30069 intel report (Beta)
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Edit Public Description
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
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 23 hours ago
TLE from 23 hours ago
0 FENGYUN 1C DEB
1 30069U 99025PW 25307.48932966 .00000624 00000-0 40805-3 0 9999
2 30069 98.7975 290.5055 0049138 161.5941 322.5953 14.05173564962959Epoch: 2025-11-03T11:44Z
TLE epoch observation values (Epoch: 2025-11-03T11:44:38.082Z)
Latitude
55.26204°
Longitude
-95.81588°
Altitude
856.801 km
Speed
7.444 km/s
True Right ascension
08h 13m 19s
True Declination
55° 06' 11"
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
06:27:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
908.749 km
Perigee altitude
837.486 km
Semi-major axis
7,251.255 km
Eccentricity
0.00491
Inclination
98.7975°
RAAN
290.5055°
Arg. of periapsis
161.5941°
True anomaly
322.25159°
Mean anomaly
322.5953°
Eccentric anomaly
322.42361°
Mean motion
3.51498 °/min
Orbital period
102.42 mins
BSTAR
0.00040805
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2025-11-04 11:39:44.240Z | 20.142° NNE | 2025-11-04 11:44:44.240Z | 102.093° ESE | 42.464° | 2025-11-04 11:49:44.240Z | 183.827° SSW |
| 4 mins | 2025-11-04 13:23:44.240Z | 319.901° NNW | 2025-11-04 13:25:44.240Z | 294.01° NW | 16.055° | 2025-11-04 13:27:44.240Z | 269.759° W |
| 5 mins | 2025-11-04 21:31:44.240Z | 81.721° E | 2025-11-04 21:33:44.240Z | 56.717° ENE | 16.393° | 2025-11-04 21:36:44.240Z | 23.703° NE |
| 9 mins | 2025-11-04 23:09:44.240Z | 176.149° S | 2025-11-04 23:13:44.240Z | 236.649° WSW | 43.034° | 2025-11-04 23:18:44.240Z | 340.114° N |
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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