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, Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 9 hours ago
TLE from 9 hours ago
0 CENTISPACE-1 S14
1 62583U 25007J 26202.23654695 -.00000092 00000-0 45591-4 0 9990
2 62583 54.9826 173.5244 0011615 151.2478 208.9120 13.80615571 79418Epoch: 2026-07-21T05:40Z
TLE epoch observation values (Epoch: 2026-07-21T05:40:37.656Z)
Latitude
-0.00007°
Longitude
149.35832°
Altitude
970.191 km
Speed
7.364 km/s
True Right ascension
11h 34m 05s
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
03:19:55
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
970.197 km
Perigee altitude
953.147 km
Semi-major axis
7,339.809 km
Eccentricity
0.00116
Inclination
54.9826°
RAAN
173.5244°
Arg. of periapsis
151.2478°
True anomaly
208.84773°
Mean anomaly
208.912°
Eccentric anomaly
208.87986°
Mean motion
3.45156 °/min
Orbital period
104.3 mins
BSTAR
0.000045591
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2026-07-21 23:10:55.990Z | 166.437° S | 2026-07-21 23:14:55.990Z | 121.027° SE | 22.117° | 2026-07-21 23:18:55.990Z | 76.453° E |
| 11 mins | 2026-07-22 00:57:55.990Z | 234.472° WSW | 2026-07-22 01:02:55.990Z | 307.468° NW | 44.005° | 2026-07-22 01:08:55.990Z | 44.36° NE |
| 8 mins | 2026-07-22 02:48:55.990Z | 293.941° NW | 2026-07-22 02:52:55.990Z | 344.202° N | 24.252° | 2026-07-22 02:56:55.990Z | 30.387° NE |
| 7 mins | 2026-07-22 04:39:55.990Z | 326.902° NNW | 2026-07-22 04:42:55.990Z | 359.647° N | 19.232° | 2026-07-22 04:46:55.990Z | 44.454° NE |
| 10 mins | 2026-07-22 06:28:55.990Z | 326.92° NNW | 2026-07-22 06:33:55.990Z | 33.252° NE | 30.923° | 2026-07-22 06:38:55.990Z | 92.756° ESE |
| 11 mins | 2026-07-22 08:17:55.990Z | 305.068° NW | 2026-07-22 08:22:55.990Z | 219.09° SW | 41.794° | 2026-07-22 08:28:55.990Z | 148.714° 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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