FENGYUN 1C DEB, 30326
Orbit data source: Space-Track
FENGYUN 1C DEB, 30326 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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30326 intel report (Beta)
FENGYUN 1C DEB details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 17 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 17 hours ago
0 FENGYUN 1C DEB
1 30326U 99025AAM 25025.18052608 .00000295 00000-0 27179-3 0 9998
2 30326 98.6840 296.5022 0141669 185.7016 174.2534 13.85294058910036Epoch: 2025-01-25T04:19Z
Definitive object data (Epoch: 2025-01-25T04:19:57.453Z)
| Latitude | -0.00007° |
| Longitude | 106.77978° |
| Altitude | 1,051.299 km |
| Speed | 7.274 km/s |
| True Right ascension | 19h 46m 00s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -19.63698° |
| Longitude | -75.68841° |
| Altitude | 852.659 km |
| Speed | 7.476 km/s |
| Apparent Right ascension | 08h 41m 57s |
| Apparent Declination | -30° 26' 53" |
| Sunlit | Object is in full shadow |
Visualization observer readout
| Local Sidereal Time | 22:14:45 |
| Azimuth | 70.574° E |
| Elevation | -68.893° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 1,046.081 km |
| Perigee altitude | 838.663 km |
| Semi-major axis | 7,320.509 km |
| Eccentricity | 0.0141669 |
| Inclination | 98.684° |
| RAAN | 296.5022° |
| Arg. of periapsis | 185.7016° |
| True anomaly | 174.41313° |
| Mean anomaly | 174.2534° |
| Eccentric anomaly | 174.33355° |
| Mean motion | 3.46522 °/min |
| BSTAR | 0.00027179 |
| Orbital period | 103.89 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 | 2025-01-26 06:56:34.603Z | 11.348° NNE | 2025-01-26 07:00:34.603Z | 299.064° NW | 44.814° | 2025-01-26 07:05:34.603Z | 198.068° SSW |
| 8 mins | 2025-01-26 16:53:34.603Z | 114.108° SE | 2025-01-26 16:57:34.603Z | 59.332° ENE | 27.494° | 2025-01-26 17:01:34.603Z | 11.983° NNE |
| 10 mins | 2025-01-26 18:34:34.603Z | 195.396° SSW | 2025-01-26 18:39:34.603Z | 260.812° W | 34.338° | 2025-01-26 18:44:34.603Z | 328.469° NNW |
Authenticating...
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