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: 5 hours ago
TLE from 5 hours ago
0 CENTISPACE-1 S12
1 62581U 25007G 26262.51147388 -.00000077 00000-0 60573-4 0 9991
2 62581 54.9782 321.4878 0013751 318.0691 41.9212 13.80621753 87760Epoch: 2026-09-19T12:16Z
TLE epoch observation values (Epoch: 2026-09-19T12:16:31.343Z)
Latitude
0.00004°
Longitude
138.93828°
Altitude
955.2 km
Speed
7.379 km/s
True Right ascension
21h 25m 57s
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
10:05:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
971.744 km
Perigee altitude
951.558 km
Semi-major axis
7,339.788 km
Eccentricity
0.00138
Inclination
54.9782°
RAAN
321.4878°
Arg. of periapsis
318.0691°
True anomaly
42.02661°
Mean anomaly
41.9212°
Eccentric anomaly
41.97389°
Mean motion
3.45158 °/min
Orbital period
104.3 mins
BSTAR
0.000060573
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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 | 2026-09-20 05:46:17.904Z | 198.462° SSW | 2026-09-20 05:52:17.904Z | 122.523° SE | 45.827° | 2026-09-20 05:57:17.904Z | 59.98° ENE |
| 10 mins | 2026-09-20 07:36:17.904Z | 260.072° W | 2026-09-20 07:41:17.904Z | 339.321° N | 45.458° | 2026-09-20 07:46:17.904Z | 37.478° NE |
| 8 mins | 2026-09-20 09:27:17.904Z | 308.463° NW | 2026-09-20 09:31:17.904Z | 353.722° N | 21.942° | 2026-09-20 09:35:17.904Z | 35.581° NE |
| 8 mins | 2026-09-20 11:18:17.904Z | 333.82° NNW | 2026-09-20 11:21:17.904Z | 8.231° NNE | 23.701° | 2026-09-20 11:26:17.904Z | 63.782° ENE |
| 10 mins | 2026-09-20 13:07:17.904Z | 323.965° NNW | 2026-09-20 13:11:17.904Z | 21.253° NNE | 56.381° | 2026-09-20 13:17:17.904Z | 113.99° SE |
| 9 mins | 2026-09-20 14:56:17.904Z | 287.614° WNW | 2026-09-20 15:00:17.904Z | 232.767° WSW | 34.518° | 2026-09-20 15:05:17.904Z | 174.752° 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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