CHUANG XIN 16A (CX-16A), 53586
Orbit data source: Space-Track
CHUANG XIN 16A (CX-16A), 53586 is a payload satellite owned by IMI/CAS (CN) in LEO that was launched on Tue, 23 Aug 2022 UTC via a KUAIZHOU-1A launch vehicle from the Xichang Space Center, China (XSC). 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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53586 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
IMI/CAS
Mission
Operational Civil Technology
Bus & Motor
CX16, Unknown motor
Mass
100 kg wet, ~100 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 1 Pan, 1.0 m
Radar Cross Section
0.763 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 21 hours ago
TLE from 21 hours ago
0 CHUANG XIN 16A (CX-16A)
1 53586U 22102A 26172.56487007 .00001400 00000-0 83328-4 0 9992
2 53586 28.9958 297.3618 0005072 58.5202 301.5893 15.05941228210180Epoch: 2026-06-21T13:33Z
TLE epoch observation values (Epoch: 2026-06-21T13:33:24.774Z)
Latitude
0.00001°
Longitude
-175.75472°
Altitude
545.1 km
Speed
7.593 km/s
True Right ascension
19h 49m 26s
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
21:38:30
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
556.257 km
Perigee altitude
549.226 km
Semi-major axis
6,930.878 km
Eccentricity
0.00051
Inclination
28.9958°
RAAN
297.3618°
Arg. of periapsis
58.5202°
True anomaly
301.53977°
Mean anomaly
301.5893°
Eccentric anomaly
301.56454°
Mean motion
3.7615 °/min
Orbital period
95.71 mins
BSTAR
0.000083328
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Other satellites on launch #102 in the year 2022 (2022-08-23 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.CHUANG XIN 16A (CX-16A) Visibility forecast
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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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-22 13:45:28.116Z | 202.745° SW | 2026-06-22 13:47:28.116Z | 167.947° S | 16.309° | 2026-06-22 13:49:28.116Z | 137.556° SSE |
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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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