FENGYUN 1C DEB, 37449 (Decayed)
Orbit data source: Space-Track
FENGYUN 1C DEB, 37449 was space debris in LEO 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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37449 intel report (Beta)
FENGYUN 1C DEB details
Identifier | |
Orbit | Decayed |
Last TLE update | 6 months ago |
Origin | |
Manufacturer | Unknown |
Mission | Decayed spacecraft |
Bus & Motor | Unknown |
Mass | Unknown |
Launch date (UTC) | |
Launch vehicle | Unknown |
Launch site | |
Object type | Payload Rocket body Debris |
Shape & HBR | Unknown |
Radar Cross Section | Small (<0.1 m²) |
Expand to show TLE details & history
TLE from 6 months ago
0 FENGYUN 1C DEB
1 37449U 99025EHT 24162.66043662 .01220616 63342-3 46920-2 0 9992
2 37449 98.8199 134.9405 0032733 165.4448 194.7769 15.86557739796336
Epoch: 2024-06-10T15:51Z
Definitive object data (Epoch: 2024-06-10T15:51:01.723Z)
Latitude | -0.00006° |
Longitude | -2.30948° |
Altitude | 336.261 km |
Speed | 7.695 km/s |
True Right ascension | 08h 59m 45s |
True Declination | 0° 00' 00" |
Sunlit | Object was in daylight at TLE epoch |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
Apogee altitude | 330.776 km |
Perigee altitude | 286.999 km |
Semi-major axis | 6,687.025 km |
Eccentricity | 0.0032733 |
Inclination | 98.8199° |
RAAN | 134.9405° |
Arg. of periapsis | 165.4448° |
True anomaly | 194.68161° |
Mean anomaly | 194.7769° |
Eccentric anomaly | 194.72922° |
Mean motion | 3.96912 °/min |
BSTAR | 0.004692 |
Orbital period | 90.7 mins |
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Other satellites on launch #25 in the year 1999 (1999-05-10 UTC)
FENGYUN 1C DEB Visibility forecast
Observer location: undefined°, undefined
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. |
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