HXMT, 42758
Orbit data source: Space-Track
HXMT, 42758 is a payload satellite owned by CNSA (CN) in LEO that was launched on Thu, 15 Jun 2017 UTC via a CHANG ZHENG 4B 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.
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42758 intel report (Beta)
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Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 HXMT
1 42758U 17034A 25261.31054110 .00004282 00000-0 23569-3 0 9996
2 42758 43.0135 253.1866 0034592 228.2639 131.5248 15.14783797456371
TLE epoch observation values (Epoch: 2025-09-18T07:27:10.751Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #34 in the year 2017 (2017-06-15 UTC)
HXMT 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. |
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7 mins | 2025-09-19 02:38:25.935Z | 213.498° SW | 2025-09-19 02:41:25.935Z | 159.291° S | 30.492° | 2025-09-19 02:45:25.935Z | 82.598° E |
7 mins | 2025-09-19 04:18:25.935Z | 262.75° W | 2025-09-19 04:21:25.935Z | 347.965° N | 43.677° | 2025-09-19 04:25:25.935Z | 71.212° E |
6 mins | 2025-09-19 05:59:25.935Z | 295.478° NW | 2025-09-19 06:01:25.935Z | 357.388° N | 39.416° | 2025-09-19 06:05:25.935Z | 82.835° E |
6 mins | 2025-09-19 07:39:25.935Z | 282.64° WNW | 2025-09-19 07:41:25.935Z | 215.128° SW | 43.987° | 2025-09-19 07:45:25.935Z | 116.947° SE |
4 mins | 2025-09-19 09:19:25.935Z | 244.67° WSW | 2025-09-19 09:20:25.935Z | 226.768° WSW | 17.332° | 2025-09-19 09:23:25.935Z | 175.51° S |
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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