FENGYUN 1C DEB, 30035
Orbit data source: Space-Track
FENGYUN 1C DEB, 30035 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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30035 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: 2 days ago
TLE from 2 days ago
0 FENGYUN 1C DEB
1 30035U 99025NL 26237.40058414 .00000139 00000-0 60102-4 0 9998
2 30035 99.2785 177.0110 0115238 37.6141 90.0926 14.37087343 27962Epoch: 2026-08-25T09:36Z
TLE epoch observation values (Epoch: 2026-08-25T09:36:50.469Z)
Latitude
50.15834°
Longitude
-109.63754°
Altitude
777.172 km
Speed
7.47 km/s
True Right ascension
00h 32m 57s
True Declination
49° 59' 22"
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
14:40:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
847.621 km
Perigee altitude
682.982 km
Semi-major axis
7,143.439 km
Eccentricity
0.01152
Inclination
99.2785°
RAAN
177.011°
Arg. of periapsis
37.6141°
True anomaly
91.41298°
Mean anomaly
90.0926°
Eccentric anomaly
90.75281°
Mean motion
3.59486 °/min
Orbital period
100.14 mins
BSTAR
0.000060102
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-08-27 08:23:06.125Z | 32.711° NE | 2026-08-27 08:27:06.125Z | 89.314° E | 31.89° | 2026-08-27 08:32:06.125Z | 166.782° S |
| 6 mins | 2026-08-27 10:04:06.125Z | 329.279° NNW | 2026-08-27 10:06:06.125Z | 296.182° NW | 23.295° | 2026-08-27 10:10:06.125Z | 242.488° WSW |
| 7 mins | 2026-08-27 19:39:06.125Z | 140.331° SSE | 2026-08-27 19:42:06.125Z | 60.718° ENE | 38.667° | 2026-08-27 19:46:06.125Z | 356.28° N |
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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