FENGYUN 1C DEB, 30246
Orbit data source: Space-Track
FENGYUN 1C DEB, 30246 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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30246 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 30246U 99025XF 26254.87881705 .00000090 00000-0 15825-3 0 9996
2 30246 98.7063 4.2080 0370875 133.6438 353.3518 13.37160742957904Epoch: 2026-09-11T21:05Z
TLE epoch observation values (Epoch: 2026-09-11T21:05:29.793Z)
Latitude
52.73753°
Longitude
-111.51219°
Altitude
852.27 km
Speed
7.567 km/s
True Right ascension
13h 03m 01s
True Declination
52° 34' 26"
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
14:33:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,395.12 km
Perigee altitude
839.158 km
Semi-major axis
7,495.276 km
Eccentricity
0.03709
Inclination
98.7063°
RAAN
4.208°
Arg. of periapsis
133.6438°
True anomaly
352.83608°
Mean anomaly
353.3518°
Eccentric anomaly
353.09638°
Mean motion
3.34474 °/min
Orbital period
107.63 mins
BSTAR
0.00015825
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-09-13 06:42:18.291Z | 142.658° SSE | 2026-09-13 06:48:18.291Z | 79.755° E | 50.779° | 2026-09-13 06:54:18.291Z | 358.632° N |
| 10 mins | 2026-09-13 08:30:18.291Z | 215.265° SW | 2026-09-13 08:35:18.291Z | 268.926° W | 27.15° | 2026-09-13 08:40:18.291Z | 320.624° NNW |
| 8 mins | 2026-09-13 19:47:18.291Z | 33.464° NE | 2026-09-13 19:51:18.291Z | 116.498° SE | 46.147° | 2026-09-13 19:55:18.291Z | 170.587° S |
| 6 mins | 2026-09-13 21:34:18.291Z | 330.733° NNW | 2026-09-13 21:37:18.291Z | 289.126° WNW | 20.402° | 2026-09-13 21:40:18.291Z | 253.356° 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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