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, 1.0 m
Radar Cross Section
0.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 5 hours ago
TLE from 5 hours ago
0 CENTISPACE-1 S8
1 62577U 25007C 26262.48972661 -.00000070 00000-0 67201-4 0 9990
2 62577 54.9864 321.8202 0012497 312.2687 47.7209 13.80626296 87754Epoch: 2026-09-19T11:45Z
TLE epoch observation values (Epoch: 2026-09-19T11:45:12.379Z)
Latitude
0°
Longitude
147.1211°
Altitude
956.524 km
Speed
7.377 km/s
True Right ascension
21h 27m 16s
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
10:05:00
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
970.806 km
Perigee altitude
952.461 km
Semi-major axis
7,339.771 km
Eccentricity
0.00125
Inclination
54.9864°
RAAN
321.8202°
Arg. of periapsis
312.2687°
True anomaly
47.82697°
Mean anomaly
47.7209°
Eccentric anomaly
47.77392°
Mean motion
3.45159 °/min
Orbital period
104.3 mins
BSTAR
0.000067201
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-09-20 05:14:59.821Z | 175.972° S | 2026-09-20 05:19:59.821Z | 118.051° SE | 27.661° | 2026-09-20 05:23:59.821Z | 72.693° E |
| 11 mins | 2026-09-20 07:02:59.821Z | 240.18° WSW | 2026-09-20 07:07:59.821Z | 321.93° NNW | 67.193° | 2026-09-20 07:13:59.821Z | 42.939° NE |
| 8 mins | 2026-09-20 08:53:59.821Z | 297.512° NW | 2026-09-20 08:57:59.821Z | 346.182° N | 25.49° | 2026-09-20 09:01:59.821Z | 30.973° NE |
| 8 mins | 2026-09-20 10:44:59.821Z | 328.526° NNW | 2026-09-20 10:47:59.821Z | 1.126° NNE | 21.029° | 2026-09-20 10:52:59.821Z | 53.77° ENE |
| 10 mins | 2026-09-20 12:33:59.821Z | 326.781° NNW | 2026-09-20 12:38:59.821Z | 35.638° NE | 40.347° | 2026-09-20 12:43:59.821Z | 96.532° ESE |
| 10 mins | 2026-09-20 14:22:59.821Z | 302.119° NW | 2026-09-20 14:27:59.821Z | 218.926° SW | 56.106° | 2026-09-20 14:32:59.821Z | 155.544° 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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