FENGYUN 1C DEB, 30153
Orbit data source: Space-Track
FENGYUN 1C DEB, 30153 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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30153 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: 9 hours ago
TLE from 9 hours ago
0 FENGYUN 1C DEB
1 30153U 99025TJ 26090.23616961 .00001218 00000-0 10679-2 0 9995
2 30153 100.4727 96.9106 0200849 89.9327 332.5970 13.79050523962705Epoch: 2026-03-31T05:40Z
TLE epoch observation values (Epoch: 2026-03-31T05:40:05.054Z)
Latitude
59.83739°
Longitude
164.82863°
Altitude
846.962 km
Speed
7.501 km/s
True Right ascension
05h 13m 51s
True Declination
59° 41' 23"
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
19:56:32
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,112.037 km
Perigee altitude
817.082 km
Semi-major axis
7,342.696 km
Eccentricity
0.02008
Inclination
100.4727°
RAAN
96.9106°
Arg. of periapsis
89.9327°
True anomaly
331.51365°
Mean anomaly
332.597°
Eccentric anomaly
332.05777°
Mean motion
3.44953 °/min
Orbital period
104.36 mins
BSTAR
0.0010679
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-03-31 14:39:07.646Z | 343.334° N | 2026-03-31 14:43:07.646Z | 291.817° WNW | 20.426° | 2026-03-31 14:46:07.646Z | 255.33° W |
| 6 mins | 2026-03-31 22:58:07.646Z | 93.389° ESE | 2026-03-31 23:00:07.646Z | 67.739° E | 18.837° | 2026-03-31 23:04:07.646Z | 17.816° NNE |
| 9 mins | 2026-04-01 00:39:07.646Z | 184.264° SSW | 2026-04-01 00:43:07.646Z | 258.112° W | 39.441° | 2026-04-01 00:48:07.646Z | 334.167° NNW |
| 10 mins | 2026-04-01 13:18:07.646Z | 19.674° NNE | 2026-04-01 13:22:07.646Z | 65.157° ENE | 44.057° | 2026-04-01 13:28:07.646Z | 192.604° SSW |
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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