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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Edit Public Description
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: 21 hours ago
TLE from 21 hours ago
0 CENTISPACE-1 S14
1 62583U 25007J 25257.55361449 .00000309 00000-0 12814-3 0 9997
2 62583 54.9803 218.6645 0062966 356.1580 3.8915 14.47543048 35952Epoch: 2025-09-14T13:17Z
TLE epoch observation values (Epoch: 2025-09-14T13:17:12.291Z)
Latitude
-0.00007°
Longitude
25.59227°
Altitude
690.063 km
Speed
7.536 km/s
True Right ascension
14h 34m 39s
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
03:06:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
778.432 km
Perigee altitude
688.871 km
Semi-major axis
7,111.789 km
Eccentricity
0.0063
Inclination
54.9803°
RAAN
218.6645°
Arg. of periapsis
356.158°
True anomaly
3.94086°
Mean anomaly
3.8915°
Eccentric anomaly
3.91614°
Mean motion
3.61889 °/min
Orbital period
99.48 mins
BSTAR
0.00012814
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-09-15 22:34:12.571Z | 169.183° S | 2025-09-15 22:37:12.571Z | 126.598° SE | 20.908° | 2025-09-15 22:40:12.571Z | 81.773° E |
| 8 mins | 2025-09-16 00:17:12.571Z | 245.44° WSW | 2025-09-16 00:20:12.571Z | 304.978° NW | 40.837° | 2025-09-16 00:25:12.571Z | 41.08° NE |
| 5 mins | 2025-09-16 02:03:12.571Z | 316.721° NNW | 2025-09-16 02:05:12.571Z | 347.285° N | 18.415° | 2025-09-16 02:08:12.571Z | 25.298° NE |
| 7 mins | 2025-09-16 05:32:12.571Z | 339.97° N | 2025-09-16 05:35:12.571Z | 28.959° NE | 25.847° | 2025-09-16 05:39:12.571Z | 84.583° E |
| 9 mins | 2025-09-16 07:15:12.571Z | 306.808° NW | 2025-09-16 07:19:12.571Z | 213.375° SW | 43.223° | 2025-09-16 07:24:12.571Z | 143.889° SSE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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