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). Payloads include a variety of satellites, spacecraft, and rockets 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)
SZ-17 MODULE details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 2 months ago |
| Origin | |
| Manufacturer | CAST |
| Mission | Decayed spacecraft |
| Bus & Motor | SHENZHOU OM, Unknown motor |
| Mass | ~1,842 kg wet, ~1,500 kg dry |
| Launch date (UTC) | |
| Launch vehicle | Unknown |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Unknown |
| Radar Cross Section | Large (>1 m²) |
Expand to show TLE details & history
TLE from 2 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 36708Epoch: 2024-12-18T08:40Z
Definitive object data (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 | Object was in full shadow at TLE epoch |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Visualization observer readout
| Observer readout values are unavailable because the object's trajectory could not be propagated. This is usually caused when the trajectory data is faulty or the object's orbit has decayed. |
Orbital elements
| Apogee altitude | 158.851 km |
| Perigee altitude | 156.506 km |
| Semi-major axis | 6,535.816 km |
| Eccentricity | 0.0001794 |
| 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 |
| BSTAR | 0.00030278 |
| Orbital period | 87.64 mins |
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Other satellites on launch #164 in the year 2023 (2023-10-26 UTC)
| SZ-17, 58146 (Decayed) |
| CZ-2F R/B, 58147 (Decayed) |
| SZ-17 MODULE, 59624 (Decayed) |
SZ-17 MODULE Visibility forecast
Observer location: undefined°, undefined
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