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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Edit Public Description
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: 15 hours ago
TLE from 15 hours ago
0 CENTISPACE-1 S8
1 62577U 25007C 25305.61031903 .00000139 00000-0 95298-4 0 9999
2 62577 54.9868 30.3898 0058253 84.7810 275.9817 14.39273769 42917Epoch: 2025-11-01T14:38Z
TLE epoch observation values (Epoch: 2025-11-01T14:38:51.564Z)
Latitude
-0.00003°
Longitude
129.537°
Altitude
757.856 km
Speed
7.479 km/s
True Right ascension
02h 01m 33s
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
01:16:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
802.452 km
Perigee altitude
719.278 km
Semi-major axis
7,139.002 km
Eccentricity
0.00583
Inclination
54.9868°
RAAN
30.3898°
Arg. of periapsis
84.781°
True anomaly
275.31732°
Mean anomaly
275.9817°
Eccentric anomaly
275.64956°
Mean motion
3.59821 °/min
Orbital period
100.05 mins
BSTAR
0.000095298
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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 | 2025-11-02 07:26:43.794Z | 191.292° SSW | 2025-11-02 07:30:43.794Z | 139.301° SSE | 29.397° | 2025-11-02 07:35:43.794Z | 63.274° ENE |
| 8 mins | 2025-11-02 09:11:43.794Z | 259.704° W | 2025-11-02 09:14:43.794Z | 309.434° NW | 34.126° | 2025-11-02 09:19:43.794Z | 36.184° NE |
| 4 mins | 2025-11-02 10:58:43.794Z | 323.027° NNW | 2025-11-02 11:00:43.794Z | 351.018° N | 16.083° | 2025-11-02 11:02:43.794Z | 17.326° NNE |
| 4 mins | 2025-11-02 12:44:43.794Z | 348.913° N | 2025-11-02 12:46:43.794Z | 16.161° NNE | 15.13° | 2025-11-02 12:48:43.794Z | 41.385° NE |
| 7 mins | 2025-11-02 14:28:43.794Z | 336.495° NNW | 2025-11-02 14:31:43.794Z | 33.409° NE | 31.001° | 2025-11-02 14:35:43.794Z | 96.491° ESE |
| 8 mins | 2025-11-02 16:12:43.794Z | 292.818° NW | 2025-11-02 16:15:43.794Z | 235.06° WSW | 34.987° | 2025-11-02 16:20:43.794Z | 159.159° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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