FENGYUN 1C DEB, 30322
Orbit data source: Space-Track
FENGYUN 1C DEB, 30322 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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30322 intel report (Beta)
FENGYUN 1C DEB details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 23 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 23 hours ago
0 FENGYUN 1C DEB
1 30322U 99025AAK 24355.60793963 .00002989 00000-0 17746-2 0 9992
2 30322 98.4273 232.8106 0128573 185.6588 174.3135 14.04145301911844Epoch: 2024-12-20T14:35Z
Definitive object data (Epoch: 2024-12-20T14:35:25.984Z)
| Latitude | -0.00001° |
| Longitude | -75.71868° |
| Altitude | 975.262 km |
| Speed | 7.317 km/s |
| True Right ascension | 15h 31m 14s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -14.74278° |
| Longitude | 102.95437° |
| Altitude | 794.02 km |
| Speed | 7.503 km/s |
| Apparent Right ascension | 02h 20m 38s |
| Apparent Declination | -27° 49' 26" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 12:46:48 |
| Azimuth | 294.79° NW |
| Elevation | -67.184° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 969.919 km |
| Perigee altitude | 783.365 km |
| Semi-major axis | 7,254.779 km |
| Eccentricity | 0.0128573 |
| Inclination | 98.4273° |
| RAAN | 232.8106° |
| Arg. of periapsis | 185.6588° |
| True anomaly | 174.45719° |
| Mean anomaly | 174.3135° |
| Eccentric anomaly | 174.38557° |
| Mean motion | 3.51242 °/min |
| BSTAR | 0.0017746 |
| Orbital period | 102.49 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2024-12-21 14:41:47.544Z | 103.67° ESE | 2024-12-21 14:44:47.544Z | 70.195° E | 19.881° | 2024-12-21 14:48:47.544Z | 22.341° NNE |
| 10 mins | 2024-12-21 16:21:47.544Z | 183.697° SSW | 2024-12-21 16:25:47.544Z | 243.555° WSW | 40.79° | 2024-12-21 16:31:47.544Z | 338.975° N |
| 9 mins | 2024-12-22 04:48:47.544Z | 17.532° NNE | 2024-12-22 04:52:47.544Z | 73.321° E | 43.985° | 2024-12-22 04:57:47.544Z | 188.504° SSW |
Authenticating...
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