CENTISPACE-1 S14, 62583
Orbit data source: Space-Track
CENTISPACE-1 S14, 62583 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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62583 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: 1 day ago
TLE from 1 day ago
0 CENTISPACE-1 S14
1 62583U 25007J 26083.20540717 -.00000043 00000-0 92654-4 0 9991
2 62583 54.9835 229.7483 0008671 284.0360 75.9632 13.80456487 62972Epoch: 2026-03-24T04:55Z
TLE epoch observation values (Epoch: 2026-03-24T04:55:47.179Z)
Latitude
-0.00002°
Longitude
-25.8847°
Altitude
961.751 km
Speed
7.373 km/s
True Right ascension
15h 18m 59s
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
11:27:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
968.601 km
Perigee altitude
955.871 km
Semi-major axis
7,340.373 km
Eccentricity
0.00087
Inclination
54.9835°
RAAN
229.7483°
Arg. of periapsis
284.036°
True anomaly
76.05962°
Mean anomaly
75.9632°
Eccentric anomaly
76.01141°
Mean motion
3.45117 °/min
Orbital period
104.31 mins
BSTAR
0.000092654
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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 S14 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 | 2026-03-25 10:35:40.919Z | 169.467° S | 2026-03-25 10:39:40.919Z | 127.032° SE | 22.035° | 2026-03-25 10:44:40.919Z | 72.59° E |
| 10 mins | 2026-03-25 12:23:40.919Z | 235.441° WSW | 2026-03-25 12:28:40.919Z | 355.408° N | 43.531° | 2026-03-25 12:33:40.919Z | 43.764° NE |
| 9 mins | 2026-03-25 14:13:40.919Z | 290.514° WNW | 2026-03-25 14:17:40.919Z | 337.101° NNW | 24.396° | 2026-03-25 14:22:40.919Z | 33.934° NE |
| 7 mins | 2026-03-25 16:05:40.919Z | 331.575° NNW | 2026-03-25 16:08:40.919Z | 6.22° NNE | 19.544° | 2026-03-25 16:12:40.919Z | 48.386° ENE |
| 10 mins | 2026-03-25 17:54:40.919Z | 329.868° NNW | 2026-03-25 17:58:40.919Z | 22.287° NNE | 31.112° | 2026-03-25 18:04:40.919Z | 94.926° ESE |
| 10 mins | 2026-03-25 19:43:40.919Z | 303.748° NW | 2026-03-25 19:47:40.919Z | 247.031° WSW | 41.576° | 2026-03-25 19:53:40.919Z | 149.807° 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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