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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 11 hours ago
TLE from 11 hours ago
0 CENTISPACE-1 S12
1 62581U 25007G 26201.91043728 -.00000110 00000-0 29035-4 0 9997
2 62581 54.9752 173.4359 0014646 187.2333 172.8414 13.80614387 79392Epoch: 2026-07-20T21:51Z
TLE epoch observation values (Epoch: 2026-07-20T21:51:01.780Z)
Latitude
-0.00004°
Longitude
-93.00925°
Altitude
973.396 km
Speed
7.361 km/s
True Right ascension
11h 33m 44s
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
21:36:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
972.427 km
Perigee altitude
950.928 km
Semi-major axis
7,339.814 km
Eccentricity
0.00146
Inclination
54.9752°
RAAN
173.4359°
Arg. of periapsis
187.2333°
True anomaly
172.86228°
Mean anomaly
172.8414°
Eccentric anomaly
172.85184°
Mean motion
3.45156 °/min
Orbital period
104.3 mins
BSTAR
0.000029035
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-07-21 08:50:17.070Z | 301.029° NW | 2026-07-21 08:55:17.070Z | 240.376° WSW | 36.264° | 2026-07-21 09:01:17.070Z | 160.368° S |
| 10 mins | 2026-07-22 00:04:17.070Z | 202.262° SSW | 2026-07-22 00:08:17.070Z | 141.407° SSE | 40.13° | 2026-07-22 00:14:17.070Z | 54.721° ENE |
| 10 mins | 2026-07-22 01:53:17.070Z | 269.638° W | 2026-07-22 01:57:17.070Z | 324.697° NNW | 32.515° | 2026-07-22 02:03:17.070Z | 37.973° NE |
| 8 mins | 2026-07-22 03:44:17.070Z | 314.032° NW | 2026-07-22 03:48:17.070Z | 359.215° N | 19.588° | 2026-07-22 03:52:17.070Z | 39.673° NE |
| 8 mins | 2026-07-22 05:35:17.070Z | 337.142° NNW | 2026-07-22 05:38:17.070Z | 14.4° NNE | 23.451° | 2026-07-22 05:43:17.070Z | 70.799° E |
| 11 mins | 2026-07-22 07:23:17.070Z | 318.453° NNW | 2026-07-22 07:28:17.070Z | 42.122° NE | 43.075° | 2026-07-22 07:34:17.070Z | 123.19° SE |
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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