SZ-17, 58146 (Decayed)
Orbit data source: Space-Track
SZ-17, 58146 was a payload satellite owned by ZZHGB (CN) in LEO that was launched on Thu, 26 Oct 2023 UTC via a CHANG ZHENG 2F launch vehicle 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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58146 intel report (Beta)
SZ-17 details
| Identifier | |
| Orbit | Decayed |
| Last TLE update | 9 months ago |
| Origin | |
| Manufacturer | CALT |
| Mission | Decayed Civil Spaceship |
| Bus & Motor | SHENZHOU, Unknown motor |
| Mass | ~8,100 kg wet, 3,258 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Cyl + 2 Pan, 17 m |
| Radar Cross Section | 39.234 m², Large (>1 m²) |
Expand to show TLE details & history
TLE from 9 months ago
0 SZ-17
1 58146U 23164A 24131.92201202 .00086906 00000-0 90008-3 0 9998
2 58146 41.4681 310.7607 0003738 318.2893 41.7661 15.63655876 29311Epoch: 2024-05-10T22:07Z
Definitive object data (Epoch: 2024-05-10T22:07:41.838Z)
| Latitude | -0.00005° |
| Longitude | 109.64075° |
| Altitude | 374.823 km |
| Speed | 7.688 km/s |
| True Right ascension | 20h 43m 02s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in daylight 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 | 381.869 km |
| Perigee altitude | 376.817 km |
| Semi-major axis | 6,757.48 km |
| Eccentricity | 0.0003738 |
| Inclination | 41.4681° |
| RAAN | 310.7607° |
| Arg. of periapsis | 318.2893° |
| True anomaly | 41.79464° |
| Mean anomaly | 41.7661° |
| Eccentric anomaly | 41.78037° |
| Mean motion | 3.9072 °/min |
| BSTAR | 0.00090008 |
| Orbital period | 92.14 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 Visibility forecast
Observer location: undefined°, undefined
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