CENTISPACE-1 S8, 62577
Orbit data source: Space-Track
CENTISPACE-1 S8, 62577 is a payload satellite owned by Centispace (CN) in LEO that was launched on Mon, 13 Jan 2025 UTC via a JIELONG-3 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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62577 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH Shenzhen
Mission
Operational Commercial Nav/Com
Bus & Motor
WK01, Unknown motor
Mass
140 kg wet, 140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Box + 2 Pan, 0.9 m
Radar Cross Section
0.833 m², Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 CENTISPACE-1 S8
1 62577U 25007C 26083.87171097 -.00000056 00000-0 81263-4 0 9996
2 62577 54.9841 226.3990 0009675 308.2890 51.7195 13.79766675 63080Epoch: 2026-03-24T20:55Z
TLE epoch observation values (Epoch: 2026-03-24T20:55:15.827Z)
Latitude
-0.00005°
Longitude
90.23988°
Altitude
961.339 km
Speed
7.374 km/s
True Right ascension
15h 05m 35s
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
11:24:42
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
971.786 km
Perigee altitude
957.578 km
Semi-major axis
7,342.819 km
Eccentricity
0.00097
Inclination
54.9841°
RAAN
226.399°
Arg. of periapsis
308.289°
True anomaly
51.80659°
Mean anomaly
51.7195°
Eccentric anomaly
51.76304°
Mean motion
3.44944 °/min
Orbital period
104.36 mins
BSTAR
0.000081263
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Other satellites on launch #7 in the year 2025 (2025-01-13 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 S8 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-03-25 10:57:16.905Z | 186.713° SSW | 2026-03-25 11:02:16.905Z | 126.51° SE | 30.423° | 2026-03-25 11:07:16.905Z | 65.173° ENE |
| 10 mins | 2026-03-25 12:46:16.905Z | 250.86° W | 2026-03-25 12:51:16.905Z | 337.206° NNW | 39.133° | 2026-03-25 12:56:16.905Z | 39.116° NE |
| 8 mins | 2026-03-25 14:37:16.905Z | 303.674° NW | 2026-03-25 14:41:16.905Z | 350.714° N | 21.643° | 2026-03-25 14:45:16.905Z | 33.584° NE |
| 8 mins | 2026-03-25 16:28:16.905Z | 331.122° NNW | 2026-03-25 16:32:16.905Z | 17.816° NNE | 20.675° | 2026-03-25 16:36:16.905Z | 58.747° ENE |
| 10 mins | 2026-03-25 18:17:16.905Z | 325.237° NNW | 2026-03-25 18:22:16.905Z | 43.242° NE | 36.629° | 2026-03-25 18:27:16.905Z | 105.386° ESE |
| 10 mins | 2026-03-25 20:06:16.905Z | 295.431° NW | 2026-03-25 20:10:16.905Z | 243.623° WSW | 34.185° | 2026-03-25 20:16:16.905Z | 164.601° 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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