YIJIAN, 41899
Orbit data source: Space-Track
YIJIAN, 41899 is a payload satellite owned by SECM (CN) in SSO that was launched on Wed, 21 Dec 2016 UTC via a CHANG ZHENG 2D launch vehicle from the Jiuquan Satellite Launch Center, China (JSC). 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
41899 intel report (Beta)
Create New Watchlist
Edit Public Description
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 YIJIAN
1 41899U 16081B 25312.47222362 .00001245 00000-0 26728-3 0 9998
2 41899 98.5247 298.7731 0019749 272.1057 87.7881 14.60346647472372TLE epoch observation values (Epoch: 2025-11-08T11:20:00.120Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #81 in the year 2016 (2016-12-21 UTC)
YIJIAN Visibility forecast
Loading observer location...
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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-09 22:01:15.527Z | 105.271° ESE | 2025-11-09 22:04:15.527Z | 64.943° ENE | 17.214° | 2025-11-09 22:07:15.527Z | 24.009° NE |
| 7 mins | 2025-11-09 23:38:15.527Z | 192.284° SSW | 2025-11-09 23:41:15.527Z | 253.615° W | 36.573° | 2025-11-09 23:45:15.527Z | 331.845° NNW |
| 7 mins | 2025-11-10 11:37:15.527Z | 40.656° NE | 2025-11-10 11:40:15.527Z | 109.243° ESE | 32.638° | 2025-11-10 11:44:15.527Z | 168.359° S |
| 5 mins | 2025-11-10 13:15:15.527Z | 325.357° NNW | 2025-11-10 13:17:15.527Z | 292.606° NW | 19.632° | 2025-11-10 13:20:15.527Z | 250.073° W |
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 |
|---|
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 |
|---|