GAOFEN 3, 41727
Orbit data source: Space-Track
GAOFEN 3, 41727 is a payload satellite owned by GWHYZ (CN) in SSO that was launched on Tue, 09 Aug 2016 UTC via a CHANG ZHENG 4C launch vehicle from the Taiyaun Space Center, China (TSC). Payload-class satellites include a variety of spacecraft equipped with specific instruments for various scientific and technological missions. These include communications satellites like Starlink; space stations such as the ISS; scientific satellites like the Hubble; Earth observation satellites from companies like Planet Labs, Umbra, and HawkEye 360; GPS; miniature CubeSats for education and research; and military/defense satellites.
Embed this page
41727 intel report (Beta)
Create New Watchlist
Edit Public Description
Expand to show TLE details & historyLast TLE update: 20 hours ago
TLE from 20 hours ago
0 GAOFEN 3
1 41727U 16049A 25249.25923111 .00000142 00000-0 56187-4 0 9995
2 41727 98.4058 256.3012 0000786 66.6934 293.4338 14.42238943477720
TLE epoch observation values (Epoch: 2025-09-06T06:13:17.567Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #49 in the year 2016 (2016-08-09 UTC)
GAOFEN 3 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 | 2025-09-07 12:46:07.767Z | 31.557° NE | 2025-09-07 12:51:07.767Z | 110.415° ESE | 29.556° | 2025-09-07 12:55:07.767Z | 163.233° S |
6 mins | 2025-09-07 14:27:07.767Z | 328.399° NNW | 2025-09-07 14:29:07.767Z | 293.94° NW | 23.369° | 2025-09-07 14:33:07.767Z | 239.286° WSW |
8 mins | 2025-09-07 23:59:07.767Z | 134.884° SE | 2025-09-08 00:02:07.767Z | 84.732° E | 34.052° | 2025-09-08 00:07:07.767Z | 0.897° NNE |
5 mins | 2025-09-08 01:39:07.767Z | 232.718° WSW | 2025-09-08 01:41:07.767Z | 261.833° W | 19.016° | 2025-09-08 01:44:07.767Z | 305.172° NW |
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 |
---|