FENGYUN 1C DEB, 30895
Orbit data source: Space-Track
FENGYUN 1C DEB, 30895 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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30895 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 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 30895U 99025AYH 26260.43627609 .00000444 00000-0 14259-3 0 9999
2 30895 98.6895 334.9040 0216018 24.9537 33.0538 14.32082951 17750Epoch: 2026-09-17T10:28Z
TLE epoch observation values (Epoch: 2026-09-17T10:28:14.254Z)
Latitude
58.39568°
Longitude
167.16868°
Altitude
665.913 km
Speed
7.597 km/s
True Right ascension
21h 22m 24s
True Declination
58° 14' 24"
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
10:07:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
936.586 km
Perigee altitude
627.246 km
Semi-major axis
7,160.053 km
Eccentricity
0.0216
Inclination
98.6895°
RAAN
334.904°
Arg. of periapsis
24.9537°
True anomaly
34.43504°
Mean anomaly
33.0538°
Eccentric anomaly
33.74127°
Mean motion
3.58236 °/min
Orbital period
100.49 mins
BSTAR
0.00014259
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-09-18 18:36:49.825Z | 357.227° N | 2026-09-18 18:41:49.825Z | 278.386° WNW | 41.811° | 2026-09-18 18:45:49.825Z | 224.465° SW |
| 6 mins | 2026-09-19 04:16:49.825Z | 112.799° SE | 2026-09-19 04:18:49.825Z | 74.157° E | 28.228° | 2026-09-19 04:22:49.825Z | 9.469° NNE |
| 5 mins | 2026-09-19 05:56:49.825Z | 232.484° WSW | 2026-09-19 05:58:49.825Z | 272.076° WNW | 23.267° | 2026-09-19 06:01:49.825Z | 316.549° 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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