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: 20 hours ago
TLE from 20 hours ago
0 CENTISPACE-1 S13
1 62582U 25007H 26045.21343476 -.00000021 00000-0 92235-4 0 9993
2 62582 54.9817 2.7102 0008273 287.5016 72.5042 13.94846234 57725Epoch: 2026-02-14T05:07Z
TLE epoch observation values (Epoch: 2026-02-14T05:07:20.763Z)
Latitude
-0.00005°
Longitude
141.63394°
Altitude
910.916 km
Speed
7.398 km/s
True Right ascension
00h 10m 50s
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
03:36:33
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
917.695 km
Perigee altitude
905.634 km
Semi-major axis
7,289.801 km
Eccentricity
0.00083
Inclination
54.9817°
RAAN
2.7102°
Arg. of periapsis
287.5016°
True anomaly
72.59464°
Mean anomaly
72.5042°
Eccentric anomaly
72.54942°
Mean motion
3.48714 °/min
Orbital period
103.24 mins
BSTAR
0.000092235
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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 | 2026-02-15 02:02:49.015Z | 293.639° NW | 2026-02-15 02:07:49.015Z | 349.721° N | 21.326° | 2026-02-15 02:11:49.015Z | 33.24° NE |
| 7 mins | 2026-02-15 03:53:49.015Z | 332.083° NNW | 2026-02-15 03:56:49.015Z | 6.69° NNE | 19.233° | 2026-02-15 04:00:49.015Z | 51.393° ENE |
| 9 mins | 2026-02-15 05:41:49.015Z | 328.823° NNW | 2026-02-15 05:45:49.015Z | 26.611° NE | 33.696° | 2026-02-15 05:50:49.015Z | 98.223° ESE |
| 9 mins | 2026-02-15 07:29:49.015Z | 296.57° NW | 2026-02-15 07:33:49.015Z | 227.091° WSW | 37.475° | 2026-02-15 07:38:49.015Z | 159.425° S |
| 9 mins | 2026-02-15 22:32:49.015Z | 192.794° SSW | 2026-02-15 22:36:49.015Z | 133.147° SE | 35.435° | 2026-02-15 22:41:49.015Z | 60.951° ENE |
| 10 mins | 2026-02-16 00:19:49.015Z | 258.84° W | 2026-02-16 00:24:49.015Z | 333.417° NNW | 35.034° | 2026-02-16 00:29:49.015Z | 36.955° 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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