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: 6 hours ago
TLE from 6 hours ago
0 CENTISPACE-1 S13
1 62582U 25007H 26124.49709637 -.00000084 00000-0 53973-4 0 9991
2 62582 54.9801 84.2776 0011173 8.3211 351.7929 13.80598772 68699Epoch: 2026-05-04T11:55Z
TLE epoch observation values (Epoch: 2026-05-04T11:55:49.126Z)
Latitude
0.00002°
Longitude
42.93748°
Altitude
954.668 km
Speed
7.379 km/s
True Right ascension
05h 37m 06s
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
01:38:40
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
969.933 km
Perigee altitude
953.531 km
Semi-major axis
7,339.869 km
Eccentricity
0.00112
Inclination
54.9801°
RAAN
84.2776°
Arg. of periapsis
8.3211°
True anomaly
351.7746°
Mean anomaly
351.7929°
Eccentric anomaly
351.78375°
Mean motion
3.45152 °/min
Orbital period
104.3 mins
BSTAR
0.000053973
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-05-04 22:28:38.606Z | 171.762° S | 2026-05-04 22:32:38.606Z | 129.059° SE | 22.801° | 2026-05-04 22:37:38.606Z | 72.44° E |
| 10 mins | 2026-05-05 00:16:38.606Z | 237.3° WSW | 2026-05-05 00:21:38.606Z | 344.191° N | 43.297° | 2026-05-05 00:26:38.606Z | 42.954° NE |
| 8 mins | 2026-05-05 02:07:38.606Z | 298.669° NW | 2026-05-05 02:10:38.606Z | 335.916° NNW | 23.758° | 2026-05-05 02:15:38.606Z | 33.462° NE |
| 7 mins | 2026-05-05 03:58:38.606Z | 331.104° NNW | 2026-05-05 04:01:38.606Z | 5.505° NNE | 19.518° | 2026-05-05 04:05:38.606Z | 48.459° ENE |
| 10 mins | 2026-05-05 05:47:38.606Z | 329.216° NNW | 2026-05-05 05:51:38.606Z | 21.362° NNE | 31.634° | 2026-05-05 05:57:38.606Z | 96.09° ESE |
| 10 mins | 2026-05-05 07:36:38.606Z | 302.615° NW | 2026-05-05 07:40:38.606Z | 245.676° WSW | 40.806° | 2026-05-05 07:46:38.606Z | 151.661° SSE |
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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