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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 7 hours ago
TLE from 7 hours ago
0 CENTISPACE-1 S13
1 62582U 25007H 26202.18567163 -.00000096 00000-0 42477-4 0 9990
2 62582 54.9791 172.5955 0011720 143.9941 216.1807 13.80618075 79422Epoch: 2026-07-21T04:27Z
TLE epoch observation values (Epoch: 2026-07-21T04:27:22.028Z)
Latitude
-0.00002°
Longitude
166.79472°
Altitude
969.663 km
Speed
7.364 km/s
True Right ascension
11h 30m 22s
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
23:59:54
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
970.266 km
Perigee altitude
953.062 km
Semi-major axis
7,339.801 km
Eccentricity
0.00117
Inclination
54.9791°
RAAN
172.5955°
Arg. of periapsis
143.9941°
True anomaly
216.10151°
Mean anomaly
216.1807°
Eccentric anomaly
216.1411°
Mean motion
3.45157 °/min
Orbital period
104.3 mins
BSTAR
0.000042477
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-07-21 23:41:27.350Z | 194.454° SSW | 2026-07-21 23:47:27.350Z | 117.357° SE | 33.438° | 2026-07-21 23:52:27.350Z | 60.78° ENE |
| 10 mins | 2026-07-22 01:31:27.350Z | 258.199° W | 2026-07-22 01:35:27.350Z | 318.062° NNW | 37.06° | 2026-07-22 01:41:27.350Z | 39.269° NE |
| 8 mins | 2026-07-22 03:22:27.350Z | 309.648° NW | 2026-07-22 03:25:27.350Z | 344.035° N | 20.691° | 2026-07-22 03:30:27.350Z | 37.498° NE |
| 7 mins | 2026-07-22 05:13:27.350Z | 336.36° NNW | 2026-07-22 05:16:27.350Z | 12.515° NNE | 21.273° | 2026-07-22 05:20:27.350Z | 57.853° ENE |
| 11 mins | 2026-07-22 07:01:27.350Z | 322.265° NNW | 2026-07-22 07:06:27.350Z | 34.496° NE | 38.77° | 2026-07-22 07:12:27.350Z | 112.288° ESE |
| 10 mins | 2026-07-22 08:50:27.350Z | 293.545° NW | 2026-07-22 08:55:27.350Z | 225.086° WSW | 30.811° | 2026-07-22 09:00:27.350Z | 170.151° 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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