FENGYUN 1C DEB, 30327
Orbit data source: Space-Track
FENGYUN 1C DEB, 30327 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
30327 intel report (Beta)
Create New Watchlist
Edit Public Description
Expand to show TLE details & history
TLE from 12 hours ago
0 FENGYUN 1C DEB
1 30327U 99025AAN 25199.48913410 .00002158 00000-0 10329-2 0 9999
2 30327 98.4500 101.0965 0117866 208.7212 331.6359 14.16468649943573
TLE epoch observation values (Epoch: 2025-07-18T11:44:21.186Z)
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. |
---|---|---|---|---|---|---|---|
9 mins | 2025-07-19 06:07:29.894Z | 19.886° NNE | 2025-07-19 06:12:29.894Z | 118.909° SE | 42.213° | 2025-07-19 06:16:29.894Z | 182.175° SSW |
4 mins | 2025-07-19 07:50:29.894Z | 319.586° NNW | 2025-07-19 07:52:29.894Z | 293.611° NW | 15.298° | 2025-07-19 07:54:29.894Z | 269.204° W |
4 mins | 2025-07-19 15:54:29.894Z | 78.426° E | 2025-07-19 15:56:29.894Z | 55.118° ENE | 14.982° | 2025-07-19 15:58:29.894Z | 33.188° NE |
10 mins | 2025-07-19 17:31:29.894Z | 170.226° S | 2025-07-19 17:35:29.894Z | 214.302° SW | 44.415° | 2025-07-19 17:41:29.894Z | 344.849° N |
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 |
---|