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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 CENTISPACE-1 S11
1 62580U 25007F 26083.86389252 -.00000059 00000-0 77144-4 0 9999
2 62580 54.9766 226.0101 0008854 299.4274 60.5798 13.80789049 63085Epoch: 2026-03-24T20:44Z
TLE epoch observation values (Epoch: 2026-03-24T20:44:00.313Z)
Latitude
-0.00005°
Longitude
92.67333°
Altitude
958.923 km
Speed
7.375 km/s
True Right ascension
15h 04m 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
11:21:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
967.556 km
Perigee altitude
954.56 km
Semi-major axis
7,339.195 km
Eccentricity
0.00089
Inclination
54.9766°
RAAN
226.0101°
Arg. of periapsis
299.4274°
True anomaly
60.66822°
Mean anomaly
60.5798°
Eccentric anomaly
60.62401°
Mean motion
3.452 °/min
Orbital period
104.29 mins
BSTAR
0.000077144
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-03-25 10:45:18.030Z | 179.906° S | 2026-03-25 10:50:18.030Z | 120.59° SE | 26.916° | 2026-03-25 10:55:18.030Z | 66.289° ENE |
| 11 mins | 2026-03-25 12:33:18.030Z | 243.233° WSW | 2026-03-25 12:38:18.030Z | 313.715° NW | 41.492° | 2026-03-25 12:44:18.030Z | 41.85° NE |
| 9 mins | 2026-03-25 14:24:18.030Z | 297.623° NW | 2026-03-25 14:28:18.030Z | 343.946° N | 22.65° | 2026-03-25 14:33:18.030Z | 36.807° NE |
| 8 mins | 2026-03-25 16:15:18.030Z | 327.532° NNW | 2026-03-25 16:19:18.030Z | 12.441° NNE | 20.1° | 2026-03-25 16:23:18.030Z | 54.139° ENE |
| 10 mins | 2026-03-25 18:04:18.030Z | 325.24° NNW | 2026-03-25 18:09:18.030Z | 33.689° NE | 34.406° | 2026-03-25 18:14:18.030Z | 99.166° ESE |
| 10 mins | 2026-03-25 19:53:18.030Z | 300.058° NW | 2026-03-25 19:58:18.030Z | 222.907° SW | 37.691° | 2026-03-25 20:03:18.030Z | 159.619° S |
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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