FENGYUN 1C DEB, 30704
Orbit data source: Space-Track
FENGYUN 1C DEB, 30704 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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30704 intel report (Beta)
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Edit Public Description
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 30704U 99025ARN 25361.51397779 .00000447 00000-0 31160-3 0 9993
2 30704 98.8740 359.8586 0082054 58.9964 69.5304 14.02067189963188Epoch: 2025-12-27T12:20Z
TLE epoch observation values (Epoch: 2025-12-27T12:20:07.681Z)
Latitude
49.86118°
Longitude
-90.79921°
Altitude
874.105 km
Speed
7.431 km/s
True Right ascension
12h 41m 53s
True Declination
49° 41' 40"
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
19:55:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
943.423 km
Perigee altitude
824.248 km
Semi-major axis
7,261.973 km
Eccentricity
0.00821
Inclination
98.874°
RAAN
359.8586°
Arg. of periapsis
58.9964°
True anomaly
70.41443°
Mean anomaly
69.5304°
Eccentric anomaly
69.9721°
Mean motion
3.50721 °/min
Orbital period
102.65 mins
BSTAR
0.0003116
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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 | 2025-12-27 23:49:54.882Z | 156.636° SSE | 2025-12-27 23:54:54.882Z | 40.779° NE | 43.297° | 2025-12-27 23:58:54.882Z | 351.445° N |
| 8 mins | 2025-12-28 12:18:54.882Z | 42.549° NE | 2025-12-28 12:21:54.882Z | 92.704° ESE | 31.687° | 2025-12-28 12:26:54.882Z | 163.68° S |
| 8 mins | 2025-12-28 13:59:54.882Z | 343.247° N | 2025-12-28 14:02:54.882Z | 302.736° NW | 25.524° | 2025-12-28 14:07:54.882Z | 237.527° 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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