CENTISPACE-1 S3, 53757
Orbit data source: Space-Track
CENTISPACE-1 S3, 53757 is a payload satellite owned by Centispace (CN) in LEO that was launched on Tue, 06 Sep 2022 UTC via a KUAIZHOU-1A 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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53757 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
IMI/CAS
Mission
Operational Commercial Nav/Com
Bus & Motor
WN100, Unknown motor
Mass
97 kg wet, 97 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 1.0 m
Radar Cross Section
0.833 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 CENTISPACE-1 S3
1 53757U 22108A 26171.42244306 .00000314 00000-0 10133-3 0 9991
2 53757 53.5340 41.8810 0009566 3.9650 356.1399 14.61256163202005Epoch: 2026-06-20T10:08Z
TLE epoch observation values (Epoch: 2026-06-20T10:08:19.080Z)
Latitude
-0.00005°
Longitude
-18.83583°
Altitude
683.287 km
Speed
7.52 km/s
True Right ascension
02h 47m 31s
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
23:08:37
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
696.072 km
Perigee altitude
682.551 km
Semi-major axis
7,067.448 km
Eccentricity
0.00096
Inclination
53.534°
RAAN
41.881°
Arg. of periapsis
3.965°
True anomaly
356.13251°
Mean anomaly
356.1399°
Eccentric anomaly
356.13621°
Mean motion
3.653 °/min
Orbital period
98.55 mins
BSTAR
0.00010133
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Other satellites on launch #108 in the year 2022 (2022-09-06 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.CENTISPACE-1 S3 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2026-06-22 16:27:20.387Z | 179.492° S | 2026-06-22 16:30:20.387Z | 134.025° SE | 24.665° | 2026-06-22 16:34:20.387Z | 73.041° E |
| 8 mins | 2026-06-22 18:09:20.387Z | 251.09° W | 2026-06-22 18:13:20.387Z | 340.186° N | 38.438° | 2026-06-22 18:17:20.387Z | 41.109° NE |
| 5 mins | 2026-06-22 19:54:20.387Z | 311.909° NW | 2026-06-22 19:56:20.387Z | 341.378° N | 18.51° | 2026-06-22 19:59:20.387Z | 24.731° NE |
| 4 mins | 2026-06-22 21:39:20.387Z | 346.794° N | 2026-06-22 21:40:20.387Z | 1.251° NNE | 16.407° | 2026-06-22 21:43:20.387Z | 42.983° NE |
| 7 mins | 2026-06-22 23:21:20.387Z | 329.732° NNW | 2026-06-22 23:24:20.387Z | 21.415° NNE | 30.93° | 2026-06-22 23:28:20.387Z | 93.024° ESE |
| 7 mins | 2026-06-23 01:04:20.387Z | 291.618° WNW | 2026-06-23 01:07:20.387Z | 228.928° WSW | 35.769° | 2026-06-23 01:11:20.387Z | 158.2° S |
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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