ZHUHAI-1 02, 42759
Orbit data source: Space-Track
ZHUHAI-1 02, 42759 is a payload satellite owned by Zhuhai Orbita (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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42759 intel report (Beta)
ZHUHAI-1 02 radio frequencies
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Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 ZHUHAI-1 02
1 42759U 17034B 25243.27666475 .00196349 00000-0 11099-2 0 9995
2 42759 43.0015 184.6506 0021593 160.4201 199.7503 15.77439523455594
TLE epoch observation values (Epoch: 2025-08-31T06:38:23.834Z)
Visualization orbit readout
Visualization observer readout
Orbital elements
Other satellites on launch #34 in the year 2017 (2017-06-15 UTC)
ZHUHAI-1 02 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. |
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4 mins | 2025-08-31 23:34:17.245Z | 214.175° SW | 2025-08-31 23:36:17.245Z | 158.026° S | 28.557° | 2025-08-31 23:38:17.245Z | 92.736° ESE |
4 mins | 2025-09-01 01:10:17.245Z | 274.309° WNW | 2025-09-01 01:12:17.245Z | 18.093° NNE | 38.258° | 2025-09-01 01:14:17.245Z | 66.223° ENE |
4 mins | 2025-09-01 02:46:17.245Z | 300.734° NW | 2025-09-01 02:48:17.245Z | 33.277° NE | 32.779° | 2025-09-01 02:50:17.245Z | 78.541° E |
4 mins | 2025-09-01 04:22:17.245Z | 275.943° WNW | 2025-09-01 04:23:17.245Z | 242.927° WSW | 39.271° | 2025-09-01 04:26:17.245Z | 121.068° SE |
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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Event ID | Pc | Md | Secondary | Secondary name | Country | Click to unsort rows by TCA header |
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