FENGYUN 1C DEB, 30316
Orbit data source: Space-Track
FENGYUN 1C DEB, 30316 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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30316 intel report (Beta)
FENGYUN 1C DEB details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 21 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 21 hours ago
0 FENGYUN 1C DEB
1 30316U 99025AAD 24355.72401689 .00013143 00000-0 36728-2 0 9994
2 30316 98.6527 82.0332 0043252 44.2451 316.2185 14.45746751931582Epoch: 2024-12-20T17:22Z
Definitive object data (Epoch: 2024-12-20T17:22:35.059Z)
| Latitude | 0.00001° |
| Longitude | 91.60169° |
| Altitude | 720.359 km |
| Speed | 7.507 km/s |
| True Right ascension | 05h 28m 07s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 22.30722° |
| Longitude | -83.96048° |
| Altitude | 755.53 km |
| Speed | 7.472 km/s |
| Apparent Right ascension | 20h 37m 31s |
| Apparent Declination | -11° 29' 11" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 13:03:53 |
| Azimuth | 83.838° E |
| Elevation | -25.239° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 767.469 km |
| Perigee altitude | 705.922 km |
| Semi-major axis | 7,114.833 km |
| Eccentricity | 0.0043252 |
| Inclination | 98.6527° |
| RAAN | 82.0332° |
| Arg. of periapsis | 44.2451° |
| True anomaly | 315.87423° |
| Mean anomaly | 316.2185° |
| Eccentric anomaly | 316.0465° |
| Mean motion | 3.61656 °/min |
| BSTAR | 0.0036728 |
| Orbital period | 99.54 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2024-12-21 18:51:49.692Z | 15.171° NNE | 2024-12-21 18:55:49.692Z | 87.689° E | 44.869° | 2024-12-21 19:00:49.692Z | 192.803° SSW |
| 8 mins | 2024-12-22 06:02:49.692Z | 171.141° S | 2024-12-22 06:05:49.692Z | 215.421° SW | 44.164° | 2024-12-22 06:10:49.692Z | 344.156° N |
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