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: 4 days ago
TLE from 4 days ago
0 CENTISPACE-1 S16
1 62585U 25007L 25356.57477461 .00000110 00000-0 13525-3 0 9993
2 62585 54.9836 197.6000 0008010 271.7712 88.2342 14.15228334 50175Epoch: 2025-12-22T13:47Z
TLE epoch observation values (Epoch: 2025-12-22T13:47:40.526Z)
Latitude
-0.00007°
Longitude
-100.68982°
Altitude
842.4 km
Speed
7.433 km/s
True Right ascension
13h 10m 23s
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
10:51:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
847.286 km
Perigee altitude
835.72 km
Semi-major axis
7,219.64 km
Eccentricity
0.0008
Inclination
54.9836°
RAAN
197.6°
Arg. of periapsis
271.7712°
True anomaly
88.32595°
Mean anomaly
88.2342°
Eccentric anomaly
88.28007°
Mean motion
3.5381 °/min
Orbital period
101.75 mins
BSTAR
0.00013525
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2025-12-26 14:32:49.457Z | 206.521° SW | 2025-12-26 14:38:49.457Z | 110.54° ESE | 38.541° | 2025-12-26 14:43:49.457Z | 54.948° ENE |
| 8 mins | 2025-12-26 16:20:49.457Z | 271.53° WNW | 2025-12-26 16:24:49.457Z | 337.412° NNW | 30.948° | 2025-12-26 16:28:49.457Z | 31.711° NE |
| 5 mins | 2025-12-26 18:09:49.457Z | 325.871° NNW | 2025-12-26 18:11:49.457Z | 350.849° N | 17.542° | 2025-12-26 18:14:49.457Z | 26.72° NE |
| 7 mins | 2025-12-26 19:56:49.457Z | 338.355° N | 2025-12-26 19:59:49.457Z | 16.933° NNE | 20.301° | 2025-12-26 20:03:49.457Z | 63.708° ENE |
| 9 mins | 2025-12-26 21:42:49.457Z | 323.8° NNW | 2025-12-26 21:46:49.457Z | 38.452° NE | 40.3° | 2025-12-26 21:51:49.457Z | 115.504° SE |
| 8 mins | 2025-12-26 23:28:49.457Z | 285.891° WNW | 2025-12-26 23:32:49.457Z | 228.791° WSW | 26.122° | 2025-12-26 23:36:49.457Z | 179.64° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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