FENGYUN 1C DEB, 30253
Orbit data source: Space-Track
FENGYUN 1C DEB, 30253 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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30253 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
Small (<0.1 m²)
Expand to show TLE details & historyLast TLE update: 8 hours ago
TLE from 8 hours ago
0 FENGYUN 1C DEB
1 30253U 99025XN 26071.21091024 .00002309 00000-0 21039-2 0 9994
2 30253 98.7414 156.7135 0223028 162.1453 255.9855 13.73587902952421Epoch: 2026-03-12T05:03Z
TLE epoch observation values (Epoch: 2026-03-12T05:03:42.644Z)
Latitude
54.8035°
Longitude
-101.60381°
Altitude
1,038.932 km
Speed
7.316 km/s
True Right ascension
09h 36m 45s
True Declination
54° 38' 51"
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
17:01:34
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,148.133 km
Perigee altitude
819.744 km
Semi-major axis
7,362.075 km
Eccentricity
0.0223
Inclination
98.7414°
RAAN
156.7135°
Arg. of periapsis
162.1453°
True anomaly
253.52325°
Mean anomaly
255.9855°
Eccentric anomaly
254.75263°
Mean motion
3.43592 °/min
Orbital period
104.78 mins
BSTAR
0.0021039
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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 | 2026-03-12 17:38:20.336Z | 39.674° NE | 2026-03-12 17:42:20.336Z | 93.64° ESE | 25.607° | 2026-03-12 17:46:20.336Z | 150.455° SSE |
| 8 mins | 2026-03-12 19:22:20.336Z | 348.11° N | 2026-03-12 19:26:20.336Z | 284.464° WNW | 28.633° | 2026-03-12 19:30:20.336Z | 231.915° WSW |
| 11 mins | 2026-03-13 05:22:20.336Z | 157.346° SSE | 2026-03-13 05:28:20.336Z | 33.334° NE | 43.673° | 2026-03-13 05:33:20.336Z | 350.42° N |
| 6 mins | 2026-03-13 07:09:20.336Z | 243.558° WSW | 2026-03-13 07:11:20.336Z | 263.826° W | 16.353° | 2026-03-13 07:15:20.336Z | 304.212° NW |
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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