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: 1 day ago
TLE from 1 day ago
0 CENTISPACE-1 S12
1 62581U 25007G 25338.45426194 .00000180 00000-0 14877-3 0 9991
2 62581 54.9785 265.4115 0008105 275.2366 84.7685 14.23033623 47625Epoch: 2025-12-04T10:54Z
TLE epoch observation values (Epoch: 2025-12-04T10:54:08.231Z)
Latitude
-0.00001°
Longitude
28.36673°
Altitude
815.626 km
Speed
7.447 km/s
True Right ascension
17h 41m 38s
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
12:26:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
820.909 km
Perigee altitude
809.249 km
Semi-major axis
7,193.216 km
Eccentricity
0.00081
Inclination
54.9785°
RAAN
265.4115°
Arg. of periapsis
275.2366°
True anomaly
84.861°
Mean anomaly
84.7685°
Eccentric anomaly
84.81475°
Mean motion
3.55761 °/min
Orbital period
101.19 mins
BSTAR
0.00014877
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-12-05 20:44:57.585Z | 192.413° SSW | 2025-12-05 20:49:57.585Z | 119.215° SE | 31.784° | 2025-12-05 20:53:57.585Z | 64.603° ENE |
| 9 mins | 2025-12-05 22:30:57.585Z | 258.3° W | 2025-12-05 22:34:57.585Z | 326.255° NNW | 35.672° | 2025-12-05 22:39:57.585Z | 37.414° NE |
| 6 mins | 2025-12-06 00:18:57.585Z | 314.603° NW | 2025-12-06 00:21:57.585Z | 353.358° N | 18.121° | 2025-12-06 00:24:57.585Z | 28.209° NE |
| 6 mins | 2025-12-06 02:05:57.585Z | 336.513° NNW | 2025-12-06 02:08:57.585Z | 13.816° NNE | 17.879° | 2025-12-06 02:11:57.585Z | 49.664° ENE |
| 8 mins | 2025-12-06 03:51:57.585Z | 331.633° NNW | 2025-12-06 03:54:57.585Z | 19.331° NNE | 33.905° | 2025-12-06 03:59:57.585Z | 101.805° ESE |
| 9 mins | 2025-12-06 05:36:57.585Z | 294.305° NW | 2025-12-06 05:40:57.585Z | 227.384° WSW | 33.763° | 2025-12-06 05:45:57.585Z | 162.746° 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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