FENGYUN 1C DEB, 41832
Orbit data source: Space-Track
FENGYUN 1C DEB, 41832 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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41832 intel report (Beta)
FENGYUN 1C DEB details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 15 hours ago |
| Origin | |
| Manufacturer | Unknown |
| Mission | 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 15 hours ago
0 FENGYUN 1C DEB
1 41832U 99025EYK 24361.14370270 .00007087 00000-0 32392-2 0 9996
2 41832 98.7558 61.9047 0058496 163.3017 197.0103 14.20856270423513Epoch: 2024-12-26T03:26Z
Definitive object data (Epoch: 2024-12-26T03:26:55.913Z)
| Latitude | -0.00004° |
| Longitude | -84.95559° |
| Altitude | 865.68 km |
| Speed | 7.399 km/s |
| True Right ascension | 04h 07m 37s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | -41.78347° |
| Longitude | -76.46719° |
| Altitude | 876.975 km |
| Speed | 7.393 km/s |
| Apparent Right ascension | 05h 14m 04s |
| Apparent Declination | -41° 02' 55" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 17:50:02 |
| Azimuth | 102.306° ESE |
| Elevation | -83.071° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 861.722 km |
| Perigee altitude | 777.514 km |
| Semi-major axis | 7,197.755 km |
| Eccentricity | 0.0058496 |
| Inclination | 98.7558° |
| RAAN | 61.9047° |
| Arg. of periapsis | 163.3017° |
| True anomaly | 196.81557° |
| Mean anomaly | 197.0103° |
| Eccentric anomaly | 196.9128° |
| Mean motion | 3.55425 °/min |
| BSTAR | 0.0032392 |
| Orbital period | 101.29 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2024-12-27 03:15:32.347Z | 115.904° SE | 2024-12-27 03:19:32.347Z | 58.005° ENE | 24.672° | 2024-12-27 03:23:32.347Z | 10.064° NNE |
| 8 mins | 2024-12-27 04:55:32.347Z | 203.073° SW | 2024-12-27 04:58:32.347Z | 249.131° W | 31.466° | 2024-12-27 05:03:32.347Z | 327.474° NNW |
| 8 mins | 2024-12-27 17:13:32.347Z | 13.838° NNE | 2024-12-27 17:17:32.347Z | 194.001° SSW | 44.037° | 2024-12-27 17:21:32.347Z | 194.981° SSW |
Authenticating...
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