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: 11 hours ago
TLE from 11 hours ago
0 CENTISPACE-1 S16
1 62585U 25007L 25299.26860822 .00000772 00000-0 27953-3 0 9996
2 62585 54.9868 55.8741 0008489 276.3267 83.6751 14.42738998 41987Epoch: 2025-10-26T06:26Z
TLE epoch observation values (Epoch: 2025-10-26T06:26:47.750Z)
Latitude
0°
Longitude
-75.71209°
Altitude
749.854 km
Speed
7.481 km/s
True Right ascension
03h 43m 29s
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
12:59:45
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
755.48 km
Perigee altitude
743.379 km
Semi-major axis
7,127.566 km
Eccentricity
0.00085
Inclination
54.9868°
RAAN
55.8741°
Arg. of periapsis
276.3267°
True anomaly
83.7718°
Mean anomaly
83.6751°
Eccentric anomaly
83.72345°
Mean motion
3.60688 °/min
Orbital period
99.81 mins
BSTAR
0.00027953
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-10-26 18:37:50.723Z | 298.835° NW | 2025-10-26 18:42:50.723Z | 225.579° WSW | 31.922° | 2025-10-26 18:46:50.723Z | 167.457° S |
| 7 mins | 2025-10-27 09:11:50.723Z | 172.121° S | 2025-10-27 09:14:50.723Z | 126.104° SE | 24.852° | 2025-10-27 09:18:50.723Z | 70.953° E |
| 8 mins | 2025-10-27 10:54:50.723Z | 249.266° W | 2025-10-27 10:58:50.723Z | 338.883° N | 38.994° | 2025-10-27 11:02:50.723Z | 38.013° NE |
| 6 mins | 2025-10-27 12:40:50.723Z | 308.925° NW | 2025-10-27 12:43:50.723Z | 350.567° N | 18.216° | 2025-10-27 12:46:50.723Z | 26.824° NE |
| 4 mins | 2025-10-27 14:27:50.723Z | 351.054° N | 2025-10-27 14:28:50.723Z | 4.236° NNE | 15.294° | 2025-10-27 14:31:50.723Z | 40.848° NE |
| 8 mins | 2025-10-27 16:10:50.723Z | 334° NNW | 2025-10-27 16:14:50.723Z | 40.213° NE | 27.474° | 2025-10-27 16:18:50.723Z | 91.35° ESE |
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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