FENGYUN 1C DEB, 46992
Orbit data source: Space-Track
FENGYUN 1C DEB, 46992 is 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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46992 intel report (Beta)
FENGYUN 1C DEB details
| Identifier | |
| Orbit | LEO |
| Last TLE update | 2 days 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 2 days ago
0 FENGYUN 1C DEB
1 46992U 99025EZS 24346.25640732 .00000700 00000-0 49143-3 0 9994
2 46992 98.8559 337.5404 0070641 96.9668 263.9538 14.00255790558270Epoch: 2024-12-11T06:09Z
Definitive object data (Epoch: 2024-12-11T06:09:13.592Z)
| Latitude | -0.00009° |
| Longitude | 164.78008° |
| Altitude | 901.562 km |
| Speed | 7.398 km/s |
| True Right ascension | 22h 30m 09s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight at TLE epoch |
Visualization TLE readout
| Latitude | -48.94609° |
| Longitude | -23.42061° |
| Altitude | 950.079 km |
| Speed | 7.356 km/s |
| Apparent Right ascension | 14h 48m 07s |
| Apparent Declination | -71° 59' 49" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 07:28:02 |
| Azimuth | 156.3° SSE |
| Elevation | -43.742° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 941.445 km |
| Perigee altitude | 838.758 km |
| Semi-major axis | 7,268.238 km |
| Eccentricity | 0.0070641 |
| Inclination | 98.8559° |
| RAAN | 337.5404° |
| Arg. of periapsis | 96.9668° |
| True anomaly | 263.14959° |
| Mean anomaly | 263.9538° |
| Eccentric anomaly | 263.55162° |
| Mean motion | 3.50267 °/min |
| BSTAR | 0.00049143 |
| Orbital period | 102.78 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 | 2024-12-13 11:54:21.335Z | 32.278° NE | 2024-12-13 11:58:21.335Z | 85.491° E | 32.285° | 2024-12-13 12:03:21.335Z | 164.486° S |
| 7 mins | 2024-12-13 13:37:21.335Z | 336.687° NNW | 2024-12-13 13:40:21.335Z | 291.443° WNW | 24.212° | 2024-12-13 13:44:21.335Z | 241.482° WSW |
| 9 mins | 2024-12-13 23:26:21.335Z | 158.345° S | 2024-12-13 23:30:21.335Z | 122.895° SE | 43.494° | 2024-12-13 23:35:21.335Z | 350.063° N |
Authenticating...
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