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). 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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58146 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
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
Shape & HBR
Cyl + 2 Pan, 8.5 m
Radar Cross Section
39.234 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 year ago
TLE from 1 year 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
TLE epoch observation values (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
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
07:56:08
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
381.869 km
Perigee altitude
376.817 km
Semi-major axis
6,757.48 km
Eccentricity
0.00037
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
Orbital period
92.14 mins
BSTAR
0.00090008
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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 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
Click to sort rows by RSO header in ascending order | Click to sort rows by Country header in ascending order | Click to sort rows by Type header in ascending order | Click to sort rows by Inclination Δ header in ascending order | Click to sort rows by RAAN Δ header in ascending order | Click to sort rows by Coplanar Angle header in ascending order | Click to sort rows by SMA Δ header in ascending order | Click to sort rows by Orbital period header in ascending order | Click to sort rows by <5km Md TCA header in ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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