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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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: 5 hours ago
TLE from 5 hours ago
0 CENTISPACE-1 S12
1 62581U 25007G 26124.51221125 -.00000094 00000-0 44574-4 0 9992
2 62581 54.9761 84.1353 0016565 45.4673 314.7633 13.80622699 68706Epoch: 2026-05-04T12:17Z
TLE epoch observation values (Epoch: 2026-05-04T12:17:35.051Z)
Latitude
-0.00002°
Longitude
37.33889°
Altitude
954.148 km
Speed
7.38 km/s
True Right ascension
05h 36m 32s
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
00:49:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
973.806 km
Perigee altitude
949.49 km
Semi-major axis
7,339.785 km
Eccentricity
0.00166
Inclination
54.9761°
RAAN
84.1353°
Arg. of periapsis
45.4673°
True anomaly
314.62833°
Mean anomaly
314.7633°
Eccentric anomaly
314.69583°
Mean motion
3.45158 °/min
Orbital period
104.3 mins
BSTAR
0.000044574
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-05-04 22:50:42.555Z | 185.852° SSW | 2026-05-04 22:55:42.555Z | 122.768° SE | 30.108° | 2026-05-04 23:00:42.555Z | 64.216° ENE |
| 10 mins | 2026-05-05 00:39:42.555Z | 251.814° W | 2026-05-05 00:43:42.555Z | 310.314° NW | 39.033° | 2026-05-05 00:49:42.555Z | 40.053° NE |
| 8 mins | 2026-05-05 02:30:42.555Z | 306.591° NW | 2026-05-05 02:33:42.555Z | 341.874° N | 21.346° | 2026-05-05 02:38:42.555Z | 36.226° NE |
| 7 mins | 2026-05-05 04:21:42.555Z | 335.08° NNW | 2026-05-05 04:24:42.555Z | 10.635° NNE | 20.513° | 2026-05-05 04:28:42.555Z | 54.936° ENE |
| 10 mins | 2026-05-05 06:10:42.555Z | 328.055° NNW | 2026-05-05 06:14:42.555Z | 30.136° NE | 36.534° | 2026-05-05 06:20:42.555Z | 107.195° ESE |
| 10 mins | 2026-05-05 07:58:42.555Z | 297.402° NW | 2026-05-05 08:03:42.555Z | 227.664° WSW | 34.443° | 2026-05-05 08:08:42.555Z | 165.703° 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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