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: 7 hours ago
TLE from 7 hours ago
0 CENTISPACE-1 S16
1 62585U 25007L 26085.50007985 -.00000018 00000-0 11659-3 0 9990
2 62585 54.9873 220.3943 0009620 287.6645 72.3260 13.80585126 63291Epoch: 2026-03-26T12:00Z
TLE epoch observation values (Epoch: 2026-03-26T12:00:06.899Z)
Latitude
-0.00005°
Longitude
-143.58262°
Altitude
960.696 km
Speed
7.373 km/s
True Right ascension
14h 41m 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
00:04:31
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
968.84 km
Perigee altitude
954.718 km
Semi-major axis
7,339.916 km
Eccentricity
0.00096
Inclination
54.9873°
RAAN
220.3943°
Arg. of periapsis
287.6645°
True anomaly
72.43107°
Mean anomaly
72.326°
Eccentric anomaly
72.37853°
Mean motion
3.45149 °/min
Orbital period
104.3 mins
BSTAR
0.00011659
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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 | 2026-03-26 19:30:05.295Z | 304.468° NW | 2026-03-26 19:36:05.295Z | 221.151° SW | 39.11° | 2026-03-26 19:41:05.295Z | 156.802° SSE |
| 10 mins | 2026-03-27 10:44:05.295Z | 198.301° SSW | 2026-03-27 10:49:05.295Z | 119.544° SE | 37.572° | 2026-03-27 10:54:05.295Z | 58.014° ENE |
| 10 mins | 2026-03-27 12:33:05.295Z | 263.437° W | 2026-03-27 12:38:05.295Z | 339.725° N | 34.086° | 2026-03-27 12:43:05.295Z | 37.131° NE |
| 7 mins | 2026-03-27 14:25:05.295Z | 318.613° NNW | 2026-03-27 14:28:05.295Z | 354.384° N | 20.127° | 2026-03-27 14:32:05.295Z | 36.415° NE |
| 8 mins | 2026-03-27 16:15:05.295Z | 334.071° NNW | 2026-03-27 16:19:05.295Z | 23.257° NE | 22.505° | 2026-03-27 16:23:05.295Z | 65.92° ENE |
| 10 mins | 2026-03-27 18:04:05.295Z | 322.339° NNW | 2026-03-27 18:08:05.295Z | 21.36° NNE | 41.257° | 2026-03-27 18:14:05.295Z | 117.838° SE |
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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