FENGYUN 1C DEB, 30527
Orbit data source: Space-Track
FENGYUN 1C DEB, 30527 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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30527 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: 7 hours ago
TLE from 7 hours ago
0 FENGYUN 1C DEB
1 30527U 99025AJR 26254.59658253 .00000749 00000-0 10462-2 0 9999
2 30527 100.0442 297.3620 0408478 296.9280 220.7304 13.31551923949874Epoch: 2026-09-11T14:19Z
TLE epoch observation values (Epoch: 2026-09-11T14:19:04.730Z)
Latitude
24.89263°
Longitude
-83.33417°
Altitude
1,381.667 km
Speed
7.056 km/s
True Right ascension
08h 08m 12s
True Declination
24° 46' 20"
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
13:33:12
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
1,445.28 km
Perigee altitude
831.225 km
Semi-major axis
7,516.39 km
Eccentricity
0.04085
Inclination
100.0442°
RAAN
297.362°
Arg. of periapsis
296.928°
True anomaly
217.79138°
Mean anomaly
220.7304°
Eccentric anomaly
219.24962°
Mean motion
3.33065 °/min
Orbital period
108.09 mins
BSTAR
0.0010462
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-09-12 00:34:04.610Z | 61.439° ENE | 2026-09-12 00:36:04.610Z | 45.456° ENE | 11.51° | 2026-09-12 00:38:04.610Z | 30.083° NE |
| 13 mins | 2026-09-12 02:15:04.610Z | 139.831° SSE | 2026-09-12 02:21:04.610Z | 52.151° ENE | 54.654° | 2026-09-12 02:28:04.610Z | 352.777° N |
| 10 mins | 2026-09-12 04:03:04.610Z | 218.641° SW | 2026-09-12 04:07:04.610Z | 262.017° W | 27.75° | 2026-09-12 04:13:04.610Z | 320.469° NNW |
| 15 mins | 2026-09-12 15:22:04.610Z | 24.16° NE | 2026-09-12 15:29:04.610Z | 90.133° ESE | 58.774° | 2026-09-12 15:37:04.610Z | 179.314° S |
| 13 mins | 2026-09-12 17:09:04.610Z | 355.119° N | 2026-09-12 17:15:04.610Z | 303.329° NW | 33.913° | 2026-09-12 17:22:04.610Z | 240.669° WSW |
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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