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: 8 hours ago
TLE from 8 hours ago
0 CENTISPACE-1 S10
1 62579U 25007E 26124.39558631 -.00000081 00000-0 56180-4 0 9992
2 62579 54.9882 84.5811 0011630 16.8526 343.2815 13.80595838 68687Epoch: 2026-05-04T09:29Z
TLE epoch observation values (Epoch: 2026-05-04T09:29:38.657Z)
Latitude
0.00003°
Longitude
79.88466°
Altitude
954.621 km
Speed
7.379 km/s
True Right ascension
05h 38m 19s
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
01:38:29
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
970.278 km
Perigee altitude
953.205 km
Semi-major axis
7,339.878 km
Eccentricity
0.00116
Inclination
54.9882°
RAAN
84.5811°
Arg. of periapsis
16.8526°
True anomaly
343.24311°
Mean anomaly
343.2815°
Eccentric anomaly
343.26231°
Mean motion
3.45152 °/min
Orbital period
104.3 mins
BSTAR
0.00005618
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-05-04 23:32:27.721Z | 211.07° SW | 2026-05-04 23:37:27.721Z | 143.06° SSE | 42.363° | 2026-05-04 23:43:27.721Z | 52.324° ENE |
| 10 mins | 2026-05-05 01:22:27.721Z | 273.832° WNW | 2026-05-05 01:26:27.721Z | 326.365° NNW | 30.384° | 2026-05-05 01:32:27.721Z | 37.662° NE |
| 7 mins | 2026-05-05 03:14:27.721Z | 324.548° NNW | 2026-05-05 03:17:27.721Z | 359.952° N | 19.211° | 2026-05-05 03:21:27.721Z | 40.796° NE |
| 8 mins | 2026-05-05 05:04:27.721Z | 337.27° NNW | 2026-05-05 05:07:27.721Z | 15.22° NNE | 24.572° | 2026-05-05 05:12:27.721Z | 73.73° E |
| 11 mins | 2026-05-05 06:52:27.721Z | 316.349° NNW | 2026-05-05 06:57:27.721Z | 50.878° ENE | 44.316° | 2026-05-05 07:03:27.721Z | 128.107° SE |
| 7 mins | 2026-05-05 08:42:27.721Z | 275.045° WNW | 2026-05-05 08:45:27.721Z | 239.436° WSW | 21.348° | 2026-05-05 08:49:27.721Z | 194.882° SSW |
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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