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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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: 16 hours ago
TLE from 16 hours ago
0 CENTISPACE-1 S16
1 62585U 25007L 26045.45886465 .00000011 00000-0 11815-3 0 9994
2 62585 54.9902 1.5624 0009352 270.0503 89.9388 13.93915661 57743Epoch: 2026-02-14T11:00Z
TLE epoch observation values (Epoch: 2026-02-14T11:00:45.905Z)
Latitude
-0.00002°
Longitude
51.88949°
Altitude
915.969 km
Speed
7.395 km/s
True Right ascension
00h 06m 14s
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
05:35:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
921.728 km
Perigee altitude
908.087 km
Semi-major axis
7,293.044 km
Eccentricity
0.00094
Inclination
54.9902°
RAAN
1.5624°
Arg. of periapsis
270.0503°
True anomaly
90.04597°
Mean anomaly
89.9388°
Eccentric anomaly
89.99238°
Mean motion
3.48482 °/min
Orbital period
103.31 mins
BSTAR
0.00011815
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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 | 2026-02-15 04:40:45.546Z | 335.23° NNW | 2026-02-15 04:44:45.546Z | 27.235° NE | 23.212° | 2026-02-15 04:48:45.546Z | 71.459° E |
| 11 mins | 2026-02-15 06:27:45.546Z | 317.18° NNW | 2026-02-15 06:32:45.546Z | 35.711° NE | 43.671° | 2026-02-15 06:38:45.546Z | 125.537° SE |
| 7 mins | 2026-02-15 08:16:45.546Z | 277.579° WNW | 2026-02-15 08:19:45.546Z | 240.708° WSW | 22.155° | 2026-02-15 08:23:45.546Z | 192.843° SSW |
| 6 mins | 2026-02-15 21:34:45.546Z | 147.038° SSE | 2026-02-15 21:36:45.546Z | 124.669° SE | 16.926° | 2026-02-15 21:40:45.546Z | 82.005° E |
| 10 mins | 2026-02-15 23:19:45.546Z | 225.386° WSW | 2026-02-15 23:23:45.546Z | 224.937° SW | 44.685° | 2026-02-15 23:29:45.546Z | 47.204° ENE |
| 8 mins | 2026-02-16 01:08:45.546Z | 288.118° WNW | 2026-02-16 01:12:45.546Z | 342.776° N | 25.757° | 2026-02-16 01:16:45.546Z | 30.451° NE |
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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