CENTISPACE-1 S11, 62580
Orbit data source: Space-Track
CENTISPACE-1 S11, 62580 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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62580 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, 1.0 m
Radar Cross Section
0.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 6 hours ago
TLE from 6 hours ago
0 CENTISPACE-1 S11
1 62580U 25007F 26262.48249896 -.00000047 00000-0 88354-4 0 9997
2 62580 54.9790 321.3195 0009006 285.7384 74.2579 13.80560505 87757Epoch: 2026-09-19T11:34Z
TLE epoch observation values (Epoch: 2026-09-19T11:34:47.910Z)
Latitude
0.00002°
Longitude
149.22949°
Altitude
961.133 km
Speed
7.373 km/s
True Right ascension
21h 25m 16s
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
10:04:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
968.478 km
Perigee altitude
955.257 km
Semi-major axis
7,340.005 km
Eccentricity
0.0009
Inclination
54.979°
RAAN
321.3195°
Arg. of periapsis
285.7384°
True anomaly
74.35726°
Mean anomaly
74.2579°
Eccentric anomaly
74.30758°
Mean motion
3.45143 °/min
Orbital period
104.3 mins
BSTAR
0.000088354
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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 S11 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 | 2026-09-20 05:04:59.287Z | 167.814° S | 2026-09-20 05:08:59.287Z | 123.072° SE | 24.362° | 2026-09-20 05:13:59.287Z | 70.7° E |
| 11 mins | 2026-09-20 06:51:59.287Z | 234.758° WSW | 2026-09-20 06:56:59.287Z | 295.485° NW | 73.12° | 2026-09-20 07:02:59.287Z | 43.87° NE |
| 9 mins | 2026-09-20 08:42:59.287Z | 292.929° NW | 2026-09-20 08:46:59.287Z | 341.486° N | 26.921° | 2026-09-20 08:51:59.287Z | 35.477° NE |
| 8 mins | 2026-09-20 10:33:59.287Z | 325.455° NNW | 2026-09-20 10:37:59.287Z | 9.791° NNE | 20.734° | 2026-09-20 10:41:59.287Z | 50.328° ENE |
| 9 mins | 2026-09-20 12:23:59.287Z | 331.901° NNW | 2026-09-20 12:27:59.287Z | 28.173° NE | 37.405° | 2026-09-20 12:32:59.287Z | 91.496° ESE |
| 11 mins | 2026-09-20 14:11:59.287Z | 305.643° NW | 2026-09-20 14:16:59.287Z | 233.069° WSW | 63.747° | 2026-09-20 14:22:59.287Z | 149.392° 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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