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: 1 day ago
TLE from 1 day ago
0 CENTISPACE-1 S9
1 62578U 25007D 25306.05531182 .00000138 00000-0 96498-4 0 9995
2 62578 54.9830 29.4519 0030373 110.4175 250.0074 14.39019858 42961Epoch: 2025-11-02T01:19Z
TLE epoch observation values (Epoch: 2025-11-02T01:19:38.941Z)
Latitude
-0.00003°
Longitude
-32.03691°
Altitude
770.261 km
Speed
7.466 km/s
True Right ascension
01h 57m 48s
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
07:54:28
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
783.391 km
Perigee altitude
740.02 km
Semi-major axis
7,139.842 km
Eccentricity
0.00304
Inclination
54.983°
RAAN
29.4519°
Arg. of periapsis
110.4175°
True anomaly
249.68075°
Mean anomaly
250.0074°
Eccentric anomaly
249.84403°
Mean motion
3.59758 °/min
Orbital period
100.07 mins
BSTAR
0.000096498
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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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2025-11-03 12:45:56.751Z | 338.464° N | 2025-11-03 12:48:56.751Z | 17.788° NNE | 17.004° | 2025-11-03 12:51:56.751Z | 54.841° ENE |
| 7 mins | 2025-11-03 14:30:56.751Z | 331.992° NNW | 2025-11-03 14:33:56.751Z | 35.644° NE | 36.292° | 2025-11-03 14:37:56.751Z | 106.079° ESE |
| 7 mins | 2025-11-03 16:14:56.751Z | 284.43° WNW | 2025-11-03 16:17:56.751Z | 232.851° WSW | 28.318° | 2025-11-03 16:21:56.751Z | 174.037° S |
| 7 mins | 2025-11-04 06:49:56.751Z | 176.27° S | 2025-11-04 06:52:56.751Z | 120.71° SE | 28.952° | 2025-11-04 06:56:56.751Z | 65.874° ENE |
| 8 mins | 2025-11-04 08:32:56.751Z | 256.051° W | 2025-11-04 08:36:56.751Z | 333.527° NNW | 35.904° | 2025-11-04 08:40:56.751Z | 35.282° NE |
| 5 mins | 2025-11-04 10:19:56.751Z | 318.435° NNW | 2025-11-04 10:21:56.751Z | 345.761° N | 17.037° | 2025-11-04 10:24:56.751Z | 23.869° NE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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