FENGYUN 1C DEB, 30758
Orbit data source: Space-Track
FENGYUN 1C DEB, 30758 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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30758 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: 11 hours ago
TLE from 11 hours ago
0 FENGYUN 1C DEB
1 30758U 99025ATU 26255.31086309 .00001102 00000-0 55527-3 0 9999
2 30758 99.0403 23.4091 0038390 305.6976 83.6927 14.18163651 3653Epoch: 2026-09-12T07:27Z
TLE epoch observation values (Epoch: 2026-09-12T07:27:38.570Z)
Latitude
29.47022°
Longitude
-84.95428°
Altitude
832.286 km
Speed
7.441 km/s
True Right ascension
01h 13m 06s
True Declination
29° 19' 29"
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
10:37:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
856.414 km
Perigee altitude
801.08 km
Semi-major axis
7,206.884 km
Eccentricity
0.00384
Inclination
99.0403°
RAAN
23.4091°
Arg. of periapsis
305.6976°
True anomaly
84.13018°
Mean anomaly
83.6927°
Eccentric anomaly
83.91142°
Mean motion
3.5475 °/min
Orbital period
101.48 mins
BSTAR
0.00055527
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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 | 2026-09-12 21:26:24.843Z | 16.98° NNE | 2026-09-12 21:31:24.843Z | 74.326° E | 76.287° | 2026-09-12 21:36:24.843Z | 189.547° SSW |
| 4 mins | 2026-09-12 23:09:24.843Z | 321.735° NNW | 2026-09-12 23:11:24.843Z | 297.83° NW | 15.225° | 2026-09-12 23:13:24.843Z | 274.674° WNW |
| 5 mins | 2026-09-13 07:12:24.843Z | 89.51° E | 2026-09-13 07:14:24.843Z | 64.679° ENE | 17.26° | 2026-09-13 07:17:24.843Z | 27.946° NE |
| 9 mins | 2026-09-13 08:50:24.843Z | 178.794° S | 2026-09-13 08:54:24.843Z | 260.118° W | 65.548° | 2026-09-13 08:59:24.843Z | 339.427° 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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