CENTISPACE-1 S16, 62585
Orbit data source: Space-Track
CENTISPACE-1 S16, 62585 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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62585 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
HITSAT
Mission
Operational Commercial Nav/Com
Bus & Motor
WK01H, 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: 22 hours ago
TLE from 22 hours ago
0 CENTISPACE-1 S16
1 62585U 25007L 25257.51409748 .00000484 00000-0 16569-3 0 9995
2 62585 54.9800 219.1428 0009294 289.9753 70.0234 14.50656275 35946Epoch: 2025-09-14T12:20Z
TLE epoch observation values (Epoch: 2025-09-14T12:20:18.022Z)
Latitude
-0.00002°
Longitude
40.33568°
Altitude
722.312 km
Speed
7.496 km/s
True Right ascension
14h 36m 34s
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
03:08:50
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
730.073 km
Perigee altitude
716.873 km
Semi-major axis
7,101.61 km
Eccentricity
0.00093
Inclination
54.98°
RAAN
219.1428°
Arg. of periapsis
289.9753°
True anomaly
70.12353°
Mean anomaly
70.0234°
Eccentric anomaly
70.07346°
Mean motion
3.62667 °/min
Orbital period
99.26 mins
BSTAR
0.00016569
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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 S16 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 | 2025-09-15 23:12:44.552Z | 198.566° SSW | 2025-09-15 23:16:44.552Z | 129.347° SE | 35.764° | 2025-09-15 23:20:44.552Z | 61.122° ENE |
| 8 mins | 2025-09-16 00:56:44.552Z | 268.997° W | 2025-09-16 00:59:44.552Z | 317.97° NNW | 30.406° | 2025-09-16 01:04:44.552Z | 34.738° NE |
| 5 mins | 2025-09-16 02:42:44.552Z | 324.09° NNW | 2025-09-16 02:44:44.552Z | 350.481° N | 15.423° | 2025-09-16 02:47:44.552Z | 27.032° NE |
| 5 mins | 2025-09-16 04:27:44.552Z | 345.749° N | 2025-09-16 04:29:44.552Z | 12.738° NNE | 16.41° | 2025-09-16 04:32:44.552Z | 50.812° ENE |
| 8 mins | 2025-09-16 06:10:44.552Z | 329.814° NNW | 2025-09-16 06:13:44.552Z | 18.686° NNE | 33.942° | 2025-09-16 06:18:44.552Z | 105.545° ESE |
| 7 mins | 2025-09-16 07:54:44.552Z | 283.959° WNW | 2025-09-16 07:57:44.552Z | 224.315° SW | 30.224° | 2025-09-16 08:01:44.552Z | 168.643° 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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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