FENGYUN 1C DEB, 30043
Orbit data source: Space-Track
FENGYUN 1C DEB, 30043 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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30043 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: 9 hours ago
TLE from 9 hours ago
0 FENGYUN 1C DEB
1 30043U 99025NU 26170.52428938 .00000938 00000-0 28622-3 0 9995
2 30043 98.6284 270.2347 0278538 301.4069 56.0141 14.24456286 256Epoch: 2026-06-19T12:34Z
TLE epoch observation values (Epoch: 2026-06-19T12:34:58.602Z)
Latitude
-0.00005°
Longitude
173.7385°
Altitude
705.228 km
Speed
7.559 km/s
True Right ascension
18h 00m 56s
True Declination
0° 00' 00"
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
08:48:41
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,007.613 km
Perigee altitude
607.32 km
Semi-major axis
7,185.604 km
Eccentricity
0.02785
Inclination
98.6284°
RAAN
270.2347°
Arg. of periapsis
301.4069°
True anomaly
58.71216°
Mean anomaly
56.0141°
Eccentric anomaly
57.35794°
Mean motion
3.56327 °/min
Orbital period
101.03 mins
BSTAR
0.00028622
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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 | 2026-06-20 05:34:37.172Z | 118.36° SE | 2026-06-20 05:38:37.172Z | 68.741° E | 23.82° | 2026-06-20 05:42:37.172Z | 15.582° NNE |
| 8 mins | 2026-06-20 07:15:37.172Z | 205.938° SW | 2026-06-20 07:18:37.172Z | 267.235° W | 33.514° | 2026-06-20 07:23:37.172Z | 332.042° NNW |
| 11 mins | 2026-06-20 19:30:37.172Z | 14.929° NNE | 2026-06-20 19:35:37.172Z | 42.838° NE | 44.557° | 2026-06-20 19:41:37.172Z | 192.745° SSW |
| 6 mins | 2026-06-20 21:12:37.172Z | 326.211° NNW | 2026-06-20 21:14:37.172Z | 304.965° NW | 16.295° | 2026-06-20 21:18:37.172Z | 264.262° W |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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