SZ-17 MODULE, 59624 (Decayed)
Orbit data source: Space-Track
SZ-17 MODULE, 59624 was a payload satellite owned by ZZHGB (CN) in LEO that was launched on Thu, 26 Oct 2023 UTC launched 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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59624 intel report (Beta)
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Edit Public Description
Expand to show TLE details & historyLast TLE update: 9 months ago
TLE from 9 months ago
0 SZ-17 MODULE
1 59624U 23164C 24353.36152807 .07140113 81950-5 30278-3 0 9999
2 59624 41.4570 6.9151 0001794 173.2499 274.5824 16.43931394 36708
Epoch: 2024-12-18T08:40Z
TLE epoch observation values (Epoch: 2024-12-18T08:40:36.025Z)
Latitude
41.58441°
Longitude
-123.61359°
Altitude
157.817 km
Speed
7.818 km/s
True Right ascension
06h 15m 58s
True Declination
41° 23' 53"
Sunlit
Visualization orbit readout
Latitude
Unknown
Longitude
Unknown
Altitude
Unknown
Speed
Unknown
Apparent Right ascension
Unknown
Apparent Declination
Unknown
Sunlit
Visualization observer readout
Local Sidereal Time
22:37:25
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
158.851 km
Perigee altitude
156.506 km
Semi-major axis
6,535.816 km
Eccentricity
0.00018
Inclination
41.457°
RAAN
6.9151°
Arg. of periapsis
173.2499°
True anomaly
274.56191°
Mean anomaly
274.5824°
Eccentric anomaly
274.57215°
Mean motion
4.10765 °/min
Orbital period
87.64 mins
BSTAR
0.00030278
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Other satellites on launch #164 in the year 2023 (2023-10-26 UTC)
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You can import UDL-sourced sensor .json files into the Sandbox to generate a visibility chart that accounts for multi-vendor sensor geometry.SZ-17 MODULE Visibility
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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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This satellite is decayed. |
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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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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