FENGYUN 1C DEB, 37406
Orbit data source: Space-Track
FENGYUN 1C DEB, 37406 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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37406 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: 1 day ago
TLE from 1 day ago
0 FENGYUN 1C DEB
1 37406U 99025EFY 25311.93093436 .00002846 00000-0 16455-2 0 9997
2 37406 98.4455 186.4904 0151742 4.7469 9.6007 14.04076267627441Epoch: 2025-11-07T22:20Z
TLE epoch observation values (Epoch: 2025-11-07T22:20:32.728Z)
Latitude
14.45334°
Longitude
161.80468°
Altitude
773.331 km
Speed
7.524 km/s
True Right ascension
12h 17m 14s
True Declination
14° 22' 14"
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
01:43:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
986.97 km
Perigee altitude
766.791 km
Semi-major axis
7,255.017 km
Eccentricity
0.01517
Inclination
98.4455°
RAAN
186.4904°
Arg. of periapsis
4.7469°
True anomaly
9.89623°
Mean anomaly
9.6007°
Eccentric anomaly
9.7479°
Mean motion
3.51225 °/min
Orbital period
102.5 mins
BSTAR
0.0016455
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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 | 2025-11-09 05:37:30.149Z | 349.667° N | 2025-11-09 05:41:30.149Z | 302.213° NW | 27.627° | 2025-11-09 05:46:30.149Z | 236.798° WSW |
| 8 mins | 2025-11-09 15:27:30.149Z | 147.243° SSE | 2025-11-09 15:30:30.149Z | 84.72° E | 41.44° | 2025-11-09 15:35:30.149Z | 354.335° N |
| 9 mins | 2025-11-10 03:53:30.149Z | 38.753° NE | 2025-11-10 03:57:30.149Z | 97.094° ESE | 31.17° | 2025-11-10 04:02:30.149Z | 160.596° S |
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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