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.
Embed this page
41832 intel report (Beta)
Create New Watchlist
Edit Public Description
Expand to show TLE details & history
TLE from 21 hours ago
0 FENGYUN 1C DEB
1 41832U 99025EYK 25199.11001444 .00001926 00000-0 86218-3 0 9990
2 41832 98.7404 264.1905 0053551 294.0023 65.5555 14.22986100452508
TLE epoch observation values (Epoch: 2025-07-18T02:38:25.247Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
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. |
---|---|---|---|---|---|---|---|
10 mins | 2025-07-19 04:03:46.758Z | 154.345° SSE | 2025-07-19 04:08:46.758Z | 72.281° E | 42.761° | 2025-07-19 04:13:46.758Z | 352.415° N |
4 mins | 2025-07-19 05:47:46.758Z | 251.766° W | 2025-07-19 05:48:46.758Z | 263.987° W | 14.074° | 2025-07-19 05:51:46.758Z | 299.263° NW |
7 mins | 2025-07-19 16:22:46.758Z | 48.098° ENE | 2025-07-19 16:25:46.758Z | 92.062° ESE | 25.358° | 2025-07-19 16:29:46.758Z | 148.543° SSE |
8 mins | 2025-07-19 18:02:46.758Z | 345.858° N | 2025-07-19 18:05:46.758Z | 295.749° NW | 31.152° | 2025-07-19 18:10:46.758Z | 226.616° WSW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
---|
Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
---|
Click to sort rows by Secondary header in ascending order | Click to sort rows by Secondary name header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Owner header in ascending order | Click to sort rows by Obj. Type header in ascending order | Click to sort rows by Miss dist. header in ascending order | Click to sort rows by Rel. speed header in ascending order | Click to sort rows by Apr. angle header in ascending order | Click to sort rows by TCA header in ascending order |
---|