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: 5 hours ago
TLE from 5 hours ago
0 CENTISPACE-1 S13
1 62582U 25007H 26262.49690909 -.00000070 00000-0 66337-4 0 9998
2 62582 54.9821 321.6800 0009055 270.1487 89.8432 13.80626259 87755Epoch: 2026-09-19T11:55Z
TLE epoch observation values (Epoch: 2026-09-19T11:55:32.945Z)
Latitude
0.00002°
Longitude
144.38814°
Altitude
962.676 km
Speed
7.371 km/s
True Right ascension
21h 26m 43s
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
10:05:03
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
968.281 km
Perigee altitude
954.988 km
Semi-major axis
7,339.771 km
Eccentricity
0.00091
Inclination
54.9821°
RAAN
321.68°
Arg. of periapsis
270.1487°
True anomaly
89.94696°
Mean anomaly
89.8432°
Eccentric anomaly
89.89508°
Mean motion
3.45159 °/min
Orbital period
104.3 mins
BSTAR
0.000066337
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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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-09-20 05:25:03.149Z | 185.098° SSW | 2026-09-20 05:30:03.149Z | 131.074° SE | 32.865° | 2026-09-20 05:35:03.149Z | 68.109° E |
| 11 mins | 2026-09-20 07:14:03.149Z | 247.057° WSW | 2026-09-20 07:19:03.149Z | 331.495° NNW | 58.719° | 2026-09-20 07:25:03.149Z | 41.905° NE |
| 8 mins | 2026-09-20 09:05:03.149Z | 301.647° NW | 2026-09-20 09:09:03.149Z | 349.081° N | 24.062° | 2026-09-20 09:13:03.149Z | 32.475° NE |
| 8 mins | 2026-09-20 10:56:03.149Z | 330.633° NNW | 2026-09-20 10:59:03.149Z | 3.747° NNE | 21.691° | 2026-09-20 11:04:03.149Z | 57.053° ENE |
| 10 mins | 2026-09-20 12:45:03.149Z | 326.426° NNW | 2026-09-20 12:50:03.149Z | 42.118° NE | 44.663° | 2026-09-20 12:55:03.149Z | 102.314° ESE |
| 10 mins | 2026-09-20 14:34:03.149Z | 297.47° NW | 2026-09-20 14:38:03.149Z | 243.774° WSW | 47.234° | 2026-09-20 14:44:03.149Z | 160.901° 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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