FENGYUN 1C DEB, 30177
Orbit data source: Space-Track
FENGYUN 1C DEB, 30177 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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30177 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 30177U 99025UJ 26153.73906778 .00001554 00000-0 10160-2 0 9992
2 30177 98.6389 83.5661 0449731 45.4077 12.7099 13.63372120958061Epoch: 2026-06-02T17:44Z
TLE epoch observation values (Epoch: 2026-06-02T17:44:15.456Z)
Latitude
58.33921°
Longitude
-87.89003°
Altitude
709.249 km
Speed
7.67 km/s
True Right ascension
04h 37m 31s
True Declination
58° 11' 03"
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
00:21:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,353.433 km
Perigee altitude
687.937 km
Semi-major axis
7,398.822 km
Eccentricity
0.04497
Inclination
98.6389°
RAAN
83.5661°
Arg. of periapsis
45.4077°
True anomaly
13.90929°
Mean anomaly
12.7099°
Eccentric anomaly
13.30281°
Mean motion
3.41035 °/min
Orbital period
105.56 mins
BSTAR
0.001016
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-10 19:18:56.406Z | 169.743° S | 2026-06-10 19:22:56.406Z | 247.148° WSW | 44.558° | 2026-06-10 19:26:56.406Z | 343.614° N |
| 4 mins | 2026-06-11 06:24:56.406Z | 78.48° E | 2026-06-11 06:25:56.406Z | 87.684° E | 13.519° | 2026-06-11 06:28:56.406Z | 113.587° SE |
| 12 mins | 2026-06-11 08:05:56.406Z | 15.844° NNE | 2026-06-11 08:10:56.406Z | 98.576° ESE | 44.846° | 2026-06-11 08:17:56.406Z | 192.586° SSW |
| 7 mins | 2026-06-11 09:51:56.406Z | 326.235° NNW | 2026-06-11 09:54:56.406Z | 294.763° NW | 17.581° | 2026-06-11 09:58:56.406Z | 259.792° W |
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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