CENTISPACE-1 S5, 54020
Orbit data source: Space-Track
CENTISPACE-1 S5, 54020 is a payload satellite owned by Centispace (CN) in LEO that was launched on Fri, 07 Oct 2022 UTC via a CHANG ZHENG 11 launch vehicle from the Yellow Sea Launch Area, China (YSLA). 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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54020 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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 2 days ago
TLE from 2 days ago
0 CENTISPACE-1 S5
1 54020U 22126A 26171.43148625 .00000310 00000-0 96681-4 0 9992
2 54020 54.9972 199.9776 0014668 78.4213 281.8427 14.63017482197518Epoch: 2026-06-20T10:21Z
TLE epoch observation values (Epoch: 2026-06-20T10:21:20.411Z)
Latitude
-0.00004°
Longitude
135.99632°
Altitude
682.399 km
Speed
7.518 km/s
True Right ascension
13h 19m 54s
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
21:24:11
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
693.77 km
Perigee altitude
673.054 km
Semi-major axis
7,061.549 km
Eccentricity
0.00147
Inclination
54.9972°
RAAN
199.9776°
Arg. of periapsis
78.4213°
True anomaly
281.67813°
Mean anomaly
281.8427°
Eccentric anomaly
281.76042°
Mean motion
3.65757 °/min
Orbital period
98.43 mins
BSTAR
0.000096681
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Other satellites on launch #126 in the year 2022 (2022-10-07 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 S5 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-06-22 10:23:11.436Z | 327.001° NNW | 2026-06-22 10:27:11.436Z | 32.428° NE | 32.005° | 2026-06-22 10:31:11.436Z | 100.29° ESE |
| 7 mins | 2026-06-22 12:06:11.436Z | 292.602° NW | 2026-06-22 12:09:11.436Z | 243.535° WSW | 31.12° | 2026-06-22 12:13:11.436Z | 168.818° S |
| 5 mins | 2026-06-23 02:27:11.436Z | 157.024° SSE | 2026-06-23 02:29:11.436Z | 128.355° SE | 17.842° | 2026-06-23 02:32:11.436Z | 85.162° E |
| 8 mins | 2026-06-23 04:08:11.436Z | 239.181° WSW | 2026-06-23 04:11:11.436Z | 297.75° NW | 42.632° | 2026-06-23 04:16:11.436Z | 42.973° NE |
| 5 mins | 2026-06-23 05:52:11.436Z | 303.885° NW | 2026-06-23 05:54:11.436Z | 333.089° NNW | 18.334° | 2026-06-23 05:57:11.436Z | 17.645° NNE |
| 6 mins | 2026-06-23 09:20:11.436Z | 346.715° N | 2026-06-23 09:22:11.436Z | 18.938° NNE | 21.458° | 2026-06-23 09:26:11.436Z | 77.086° E |
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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