CHUANG XIN 19 (CX-19), 58505
Orbit data source: Space-Track
CHUANG XIN 19 (CX-19), 58505 is a payload satellite owned by Zhongguo Xingwang (CN) in LEO that was launched on Tue, 05 Dec 2023 UTC via a JIELONG-3 launch vehicle from the South China Sea Launch Area (SCSLA). 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.
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58505 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 4 hours ago
TLE from 4 hours ago
0 CHUANG XIN 19 (CX-19)
1 58505U 23190A 26162.87339685 .00000058 00000-0 78373-4 0 9999
2 58505 86.5028 334.4193 0002246 96.1945 263.9454 13.39551778123984TLE epoch observation values (Epoch: 2026-06-11T20:57:41.487Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #190 in the year 2023 (2023-12-05 UTC)
CHUANG XIN 19 (CX-19) Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 12 mins | 2026-06-12 11:24:33.216Z | 155.471° SSE | 2026-06-12 11:30:33.216Z | 74.427° E | 37.158° | 2026-06-12 11:36:33.216Z | 13.547° NNE |
| 9 mins | 2026-06-12 13:14:33.216Z | 240.854° WSW | 2026-06-12 13:18:33.216Z | 288.401° WNW | 24.162° | 2026-06-12 13:23:33.216Z | 337.629° N |
| 10 mins | 2026-06-12 22:40:33.216Z | 23.457° NE | 2026-06-12 22:44:33.216Z | 71.473° E | 30.329° | 2026-06-12 22:50:33.216Z | 142.066° SSE |
| 10 mins | 2026-06-13 00:28:33.216Z | 331.235° NNW | 2026-06-13 00:32:33.216Z | 280.487° WNW | 30.863° | 2026-06-13 00:38:33.216Z | 214.595° SW |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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