CENTISPACE-1 S13, 62582
Orbit data source: Space-Track
CENTISPACE-1 S13, 62582 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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62582 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: 17 hours ago
TLE from 17 hours ago
0 CENTISPACE-1 S13
1 62582U 25007H 26135.28525381 -.00000066 00000-0 71139-4 0 9996
2 62582 54.9819 46.5519 0011959 29.0702 331.0918 13.80600524 70186Epoch: 2026-05-15T06:50Z
TLE epoch observation values (Epoch: 2026-05-15T06:50:45.929Z)
Latitude
0°
Longitude
70.84176°
Altitude
955.097 km
Speed
7.379 km/s
True Right ascension
03h 06m 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
08:28:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
970.503 km
Perigee altitude
952.948 km
Semi-major axis
7,339.863 km
Eccentricity
0.0012
Inclination
54.9819°
RAAN
46.5519°
Arg. of periapsis
29.0702°
True anomaly
331.02547°
Mean anomaly
331.0918°
Eccentric anomaly
331.05864°
Mean motion
3.45153 °/min
Orbital period
104.3 mins
BSTAR
0.000071139
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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 S13 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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-05-16 00:36:16.406Z | 320.065° NNW | 2026-05-16 00:40:16.406Z | 1.643° NNE | 19.244° | 2026-05-16 00:44:16.406Z | 45.38° ENE |
| 10 mins | 2026-05-16 02:26:16.406Z | 328.05° NNW | 2026-05-16 02:31:16.406Z | 36.101° NE | 30.38° | 2026-05-16 02:36:16.406Z | 92.375° ESE |
| 10 mins | 2026-05-16 04:15:16.406Z | 305.577° NW | 2026-05-16 04:20:16.406Z | 210.791° SW | 42.268° | 2026-05-16 04:25:16.406Z | 148.752° SSE |
| 10 mins | 2026-05-16 19:28:16.406Z | 190.538° SSW | 2026-05-16 19:33:16.406Z | 120.73° SE | 33.237° | 2026-05-16 19:38:16.406Z | 61.442° ENE |
| 10 mins | 2026-05-16 21:17:16.406Z | 257.16° W | 2026-05-16 21:21:16.406Z | 314.042° NW | 36.972° | 2026-05-16 21:27:16.406Z | 38.934° NE |
| 8 mins | 2026-05-16 23:08:16.406Z | 308.459° NW | 2026-05-16 23:11:16.406Z | 342.379° N | 20.622° | 2026-05-16 23:16:16.406Z | 36.656° NE |
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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