CENTISPACE-1 S9, 62578
Orbit data source: Space-Track
CENTISPACE-1 S9, 62578 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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62578 intel report (Beta)
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Edit Public Description
Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH Shenzhen
Mission
Operational Commercial Nav/Com
Bus & Motor
WK01, 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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 13 hours ago
TLE from 13 hours ago
0 CENTISPACE-1 S9
1 62578U 25007D 25261.32413564 .00000475 00000-0 17185-3 0 9997
2 62578 54.9815 203.6724 0064873 12.3174 347.9381 14.47515290 36497Epoch: 2025-09-18T07:46Z
TLE epoch observation values (Epoch: 2025-09-18T07:46:45.319Z)
Latitude
0.00001°
Longitude
89.49621°
Altitude
689.724 km
Speed
7.536 km/s
True Right ascension
13h 34m 41s
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
13:31:47
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
779.879 km
Perigee altitude
687.605 km
Semi-major axis
7,111.879 km
Eccentricity
0.00649
Inclination
54.9815°
RAAN
203.6724°
Arg. of periapsis
12.3174°
True anomaly
347.78151°
Mean anomaly
347.9381°
Eccentric anomaly
347.85993°
Mean motion
3.61882 °/min
Orbital period
99.48 mins
BSTAR
0.00017185
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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 S9 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2025-09-18 21:11:11.764Z | 142.47° SSE | 2025-09-18 21:13:11.764Z | 116.691° SE | 13.057° | 2025-09-18 21:15:11.764Z | 92.257° ESE |
| 8 mins | 2025-09-18 22:52:11.764Z | 225.52° WSW | 2025-09-18 22:56:11.764Z | 47.597° ENE | 43.84° | 2025-09-18 23:00:11.764Z | 47.143° ENE |
| 6 mins | 2025-09-19 00:37:11.764Z | 295.208° NW | 2025-09-19 00:40:11.764Z | 343.497° N | 21.614° | 2025-09-19 00:43:11.764Z | 24.58° NE |
| 6 mins | 2025-09-19 04:07:11.764Z | 340.42° N | 2025-09-19 04:10:11.764Z | 24.087° NE | 21.024° | 2025-09-19 04:13:11.764Z | 66.029° ENE |
| 9 mins | 2025-09-19 05:50:11.764Z | 316.172° NNW | 2025-09-19 05:54:11.764Z | 24.055° NE | 44.365° | 2025-09-19 05:59:11.764Z | 128.869° SE |
| 5 mins | 2025-09-19 07:35:11.764Z | 266.511° W | 2025-09-19 07:37:11.764Z | 239.675° WSW | 17.456° | 2025-09-19 07:40:11.764Z | 201.521° SSW |
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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