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: 1 day ago
TLE from 1 day ago
0 CHUANG XIN 16A (CX-16A)
1 53586U 22102A 26093.69135338 .00003820 00000-0 24736-3 0 9990
2 53586 28.9949 93.5028 0004637 305.4883 54.5284 15.05675597198284Epoch: 2026-04-03T16:35Z
TLE epoch observation values (Epoch: 2026-04-03T16:35:32.932Z)
Latitude
0.00003°
Longitude
12.59378°
Altitude
545.891 km
Speed
7.593 km/s
True Right ascension
06h 14m 00s
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
06:30:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
556.77 km
Perigee altitude
550.341 km
Semi-major axis
6,931.692 km
Eccentricity
0.00046
Inclination
28.9949°
RAAN
93.5028°
Arg. of periapsis
305.4883°
True anomaly
54.57169°
Mean anomaly
54.5284°
Eccentric anomaly
54.55004°
Mean motion
3.76083 °/min
Orbital period
95.72 mins
BSTAR
0.00024736
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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 | 2026-04-05 05:33:12.903Z | 202.291° SSW | 2026-04-05 05:34:12.903Z | 184.723° SSW | 17.072° | 2026-04-05 05:37:12.903Z | 137.441° 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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