CENTISPACE-1 S12, 62581
Orbit data source: Space-Track
CENTISPACE-1 S12, 62581 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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62581 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: 21 hours ago
TLE from 21 hours ago
0 CENTISPACE-1 S12
1 62581U 25007G 25287.90405312 .00000411 00000-0 15546-3 0 9994
2 62581 54.9762 99.0692 0063860 57.4839 303.2297 14.47342771 40360Epoch: 2025-10-14T21:41Z
TLE epoch observation values (Epoch: 2025-10-14T21:41:50.189Z)
Latitude
-0.00002°
Longitude
109.92427°
Altitude
710.708 km
Speed
7.514 km/s
True Right ascension
06h 36m 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
13:38:39
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
779.728 km
Perigee altitude
688.888 km
Semi-major axis
7,112.445 km
Eccentricity
0.00639
Inclination
54.9762°
RAAN
99.0692°
Arg. of periapsis
57.4839°
True anomaly
302.6149°
Mean anomaly
303.2297°
Eccentric anomaly
302.92257°
Mean motion
3.61838 °/min
Orbital period
99.49 mins
BSTAR
0.00015546
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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 S12 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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-10-15 19:41:52.965Z | 332.146° NNW | 2025-10-15 19:45:52.965Z | 30.349° NE | 23.513° | 2025-10-15 19:48:52.965Z | 75.273° E |
| 8 mins | 2025-10-15 21:25:52.965Z | 309.12° NW | 2025-10-15 21:29:52.965Z | 192.24° SSW | 43.966° | 2025-10-15 21:33:52.965Z | 141.03° SSE |
| 8 mins | 2025-10-16 13:38:52.965Z | 217.976° SW | 2025-10-16 13:41:52.965Z | 185.379° SSW | 43.085° | 2025-10-16 13:46:52.965Z | 49.999° ENE |
| 6 mins | 2025-10-16 15:23:52.965Z | 293.243° NW | 2025-10-16 15:25:52.965Z | 325.97° NNW | 22.885° | 2025-10-16 15:29:52.965Z | 26.528° NE |
| 5 mins | 2025-10-16 18:54:52.965Z | 355.006° N | 2025-10-16 18:56:52.965Z | 26.599° NE | 18.67° | 2025-10-16 18:59:52.965Z | 65.277° ENE |
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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