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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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: 12 hours ago
TLE from 12 hours ago
0 CENTISPACE-1 S10
1 62579U 25007E 26050.28199721 -.00000044 00000-0 78908-4 0 9990
2 62579 54.9908 344.5274 0008930 260.3312 99.6641 13.91639790 58435Epoch: 2026-02-19T06:46Z
TLE epoch observation values (Epoch: 2026-02-19T06:46:04.558Z)
Latitude
-0.00003°
Longitude
93.77286°
Altitude
925.018 km
Speed
7.39 km/s
True Right ascension
22h 58m 06s
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
21:48:44
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
929.376 km
Perigee altitude
916.337 km
Semi-major axis
7,300.993 km
Eccentricity
0.00089
Inclination
54.9908°
RAAN
344.5274°
Arg. of periapsis
260.3312°
True anomaly
99.76496°
Mean anomaly
99.6641°
Eccentric anomaly
99.71453°
Mean motion
3.47913 °/min
Orbital period
103.47 mins
BSTAR
0.000078908
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-02-19 20:41:17.153Z | 168.991° S | 2026-02-19 20:45:17.153Z | 121.737° SE | 22.825° | 2026-02-19 20:49:17.153Z | 75.369° E |
| 10 mins | 2026-02-19 22:28:17.153Z | 238.332° WSW | 2026-02-19 22:32:17.153Z | 297.642° NW | 43.215° | 2026-02-19 22:38:17.153Z | 43.507° NE |
| 8 mins | 2026-02-20 00:18:17.153Z | 300.876° NW | 2026-02-20 00:21:17.153Z | 339.952° N | 23.336° | 2026-02-20 00:26:17.153Z | 35.277° NE |
| 7 mins | 2026-02-20 02:08:17.153Z | 332.461° NNW | 2026-02-20 02:11:17.153Z | 7.645° NNE | 18.815° | 2026-02-20 02:15:17.153Z | 49.691° ENE |
| 9 mins | 2026-02-20 03:56:17.153Z | 329.757° NNW | 2026-02-20 04:00:17.153Z | 22.933° NE | 30.658° | 2026-02-20 04:05:17.153Z | 90.793° ESE |
| 10 mins | 2026-02-20 05:44:17.153Z | 303.962° NW | 2026-02-20 05:48:17.153Z | 249.348° W | 41.207° | 2026-02-20 05:54:17.153Z | 149.854° 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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