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 25260.03331510 .00000350 00000-0 13710-3 0 9997
2 62579 54.9847 207.7589 0064014 0.1501 359.9495 14.48199144 36321Epoch: 2025-09-17T00:47Z
TLE epoch observation values (Epoch: 2025-09-17T00:47:58.424Z)
Latitude
-0.00001°
Longitude
-160.44961°
Altitude
687.079 km
Speed
7.538 km/s
True Right ascension
13h 51m 02s
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
20:25:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
777.014 km
Perigee altitude
685.991 km
Semi-major axis
7,109.64 km
Eccentricity
0.0064
Inclination
54.9847°
RAAN
207.7589°
Arg. of periapsis
0.1501°
True anomaly
359.94885°
Mean anomaly
359.9495°
Eccentric anomaly
359.94917°
Mean motion
3.62053 °/min
Orbital period
99.43 mins
BSTAR
0.0001371
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-19 04:36:37.175Z | 328.23° NNW | 2025-09-19 04:40:37.175Z | 21.801° NNE | 27.333° | 2025-09-19 04:45:37.175Z | 92.114° ESE |
| 9 mins | 2025-09-19 06:20:37.175Z | 304.311° NW | 2025-09-19 06:24:37.175Z | 233.56° WSW | 41.175° | 2025-09-19 06:29:37.175Z | 149.222° SSE |
| 8 mins | 2025-09-19 22:33:37.175Z | 229.014° WSW | 2025-09-19 22:36:37.175Z | 311.267° NW | 44.895° | 2025-09-19 22:41:37.175Z | 46.262° ENE |
| 6 mins | 2025-09-20 00:18:37.175Z | 303.133° NW | 2025-09-20 00:20:37.175Z | 335.417° NNW | 21.219° | 2025-09-20 00:24:37.175Z | 28.82° NE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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