CENTISPACE-1 S10, 62579
Orbit data source: Space-Track
CENTISPACE-1 S10, 62579 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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62579 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, 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 S10
1 62579U 25007E 25256.37544111 .00000296 00000-0 12197-3 0 9999
2 62579 54.9849 222.0617 0063410 354.1397 5.8842 14.48728552 35793Epoch: 2025-09-13T09:00Z
TLE epoch observation values (Epoch: 2025-09-13T09:00:38.111Z)
Latitude
-0.00001°
Longitude
94.29319°
Altitude
686.028 km
Speed
7.538 km/s
True Right ascension
14h 48m 14s
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
03:04:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
774.842 km
Perigee altitude
684.699 km
Semi-major axis
7,107.908 km
Eccentricity
0.00634
Inclination
54.9849°
RAAN
222.0617°
Arg. of periapsis
354.1397°
True anomaly
5.95928°
Mean anomaly
5.8842°
Eccentric anomaly
5.92168°
Mean motion
3.62185 °/min
Orbital period
99.4 mins
BSTAR
0.00012197
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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 S10 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 | 2025-09-15 22:24:35.672Z | 169.743° S | 2025-09-15 22:27:35.672Z | 131.354° SE | 19.113° | 2025-09-15 22:31:35.672Z | 76.693° E |
| 8 mins | 2025-09-16 00:07:35.672Z | 241.356° WSW | 2025-09-16 00:10:35.672Z | 289.326° WNW | 41.341° | 2025-09-16 00:15:35.672Z | 41.649° NE |
| 5 mins | 2025-09-16 01:53:35.672Z | 314.64° NW | 2025-09-16 01:55:35.672Z | 345.762° N | 18.865° | 2025-09-16 01:58:35.672Z | 24.609° NE |
| 7 mins | 2025-09-16 05:22:35.672Z | 341.486° N | 2025-09-16 05:25:35.672Z | 30.444° NE | 24.736° | 2025-09-16 05:29:35.672Z | 83.361° E |
| 8 mins | 2025-09-16 07:05:35.672Z | 308.522° NW | 2025-09-16 07:09:35.672Z | 190.663° SSW | 43.775° | 2025-09-16 07:13:35.672Z | 141.863° SSE |
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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