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: 17 hours ago
TLE from 17 hours ago
0 CENTISPACE-1 S14
1 62583U 25007J 25305.52656382 .00000145 00000-0 97716-4 0 9994
2 62583 54.9829 31.7504 0049224 99.2725 261.3829 14.39286074 42885Epoch: 2025-11-01T12:38Z
TLE epoch observation values (Epoch: 2025-11-01T12:38:15.114Z)
Latitude
-0.00006°
Longitude
161.13201°
Altitude
767.343 km
Speed
7.469 km/s
True Right ascension
02h 07m 00s
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
01:18:02
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
795.966 km
Perigee altitude
725.684 km
Semi-major axis
7,138.962 km
Eccentricity
0.00492
Inclination
54.9829°
RAAN
31.7504°
Arg. of periapsis
99.2725°
True anomaly
260.82572°
Mean anomaly
261.3829°
Eccentric anomaly
261.10426°
Mean motion
3.59824 °/min
Orbital period
100.05 mins
BSTAR
0.000097716
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-02 07:06:30.669Z | 168.783° S | 2025-11-02 07:09:30.669Z | 128.964° SE | 20.953° | 2025-11-02 07:13:30.669Z | 75.358° E |
| 9 mins | 2025-11-02 08:49:30.669Z | 241.045° WSW | 2025-11-02 08:53:30.669Z | 319.346° NNW | 41.91° | 2025-11-02 08:58:30.669Z | 42.049° NE |
| 5 mins | 2025-11-02 10:36:30.669Z | 311.595° NW | 2025-11-02 10:38:30.669Z | 341.291° N | 18.946° | 2025-11-02 10:41:30.669Z | 21.9° NNE |
| 6 mins | 2025-11-02 14:07:30.669Z | 345.269° N | 2025-11-02 14:09:30.669Z | 18.361° NNE | 24.822° | 2025-11-02 14:13:30.669Z | 80.786° E |
| 8 mins | 2025-11-02 15:50:30.669Z | 307.059° NW | 2025-11-02 15:54:30.669Z | 218.183° SW | 43.173° | 2025-11-02 15:58:30.669Z | 145.335° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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