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 25308.47842605 .00000111 00000-0 89301-4 0 9998
2 62581 54.9818 19.3033 0032104 72.5147 287.9340 14.38172646 43332Epoch: 2025-11-04T11:28Z
TLE epoch observation values (Epoch: 2025-11-04T11:28:56.010Z)
Latitude
-0.00006°
Longitude
163.10501°
Altitude
758.598 km
Speed
7.48 km/s
True Right ascension
01h 17m 12s
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
09:53:05
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
787.44 km
Perigee altitude
741.579 km
Semi-major axis
7,142.646 km
Eccentricity
0.00321
Inclination
54.9818°
RAAN
19.3033°
Arg. of periapsis
72.5147°
True anomaly
287.58356°
Mean anomaly
287.934°
Eccentric anomaly
287.75882°
Mean motion
3.59546 °/min
Orbital period
100.13 mins
BSTAR
0.000089301
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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 | 2025-11-05 14:41:21.744Z | 310.397° NW | 2025-11-05 14:46:21.744Z | 196.414° SSW | 44.244° | 2025-11-05 14:51:21.744Z | 139.84° SSE |
| 9 mins | 2025-11-06 07:01:21.744Z | 222.395° SW | 2025-11-06 07:05:21.744Z | 95.226° ESE | 44.756° | 2025-11-06 07:10:21.744Z | 48.238° ENE |
| 6 mins | 2025-11-06 08:47:21.744Z | 294.07° NW | 2025-11-06 08:50:21.744Z | 343.044° N | 23.069° | 2025-11-06 08:53:21.744Z | 24.445° NE |
| 4 mins | 2025-11-06 10:34:21.744Z | 340.313° N | 2025-11-06 10:35:21.744Z | 353.142° N | 14.399° | 2025-11-06 10:38:21.744Z | 29.951° NE |
| 6 mins | 2025-11-06 12:19:21.744Z | 347.096° N | 2025-11-06 12:21:21.744Z | 16.884° NNE | 20.794° | 2025-11-06 12:25:21.744Z | 70.565° E |
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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