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: 22 hours ago
TLE from 22 hours ago
0 CENTISPACE-1 S9
1 62578U 25007D 25257.52609292 .00000314 00000-0 12943-3 0 9998
2 62578 54.9811 218.5054 0064511 3.9945 356.1544 14.47509821 35940Epoch: 2025-09-14T12:37Z
TLE epoch observation values (Epoch: 2025-09-14T12:37:34.428Z)
Latitude
0.00001°
Longitude
35.36812°
Altitude
689.072 km
Speed
7.537 km/s
True Right ascension
14h 34m 01s
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
03:09:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
779.64 km
Perigee altitude
687.881 km
Semi-major axis
7,111.897 km
Eccentricity
0.00645
Inclination
54.9811°
RAAN
218.5054°
Arg. of periapsis
3.9945°
True anomaly
356.10442°
Mean anomaly
356.1544°
Eccentric anomaly
356.12945°
Mean motion
3.6188 °/min
Orbital period
99.48 mins
BSTAR
0.00012943
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2025-09-15 23:34:42.604Z | 216.539° SW | 2025-09-15 23:39:42.604Z | 97.008° ESE | 42.568° | 2025-09-15 23:43:42.604Z | 51.53° ENE |
| 6 mins | 2025-09-16 01:20:42.604Z | 290.419° WNW | 2025-09-16 01:22:42.604Z | 323.175° NNW | 24.158° | 2025-09-16 01:26:42.604Z | 25.801° NE |
| 4 mins | 2025-09-16 03:06:42.604Z | 336.277° NNW | 2025-09-16 03:08:42.604Z | 2.567° NNE | 14.131° | 2025-09-16 03:10:42.604Z | 26.558° NE |
| 5 mins | 2025-09-16 04:51:42.604Z | 352.872° N | 2025-09-16 04:53:42.604Z | 23.15° NE | 19.154° | 2025-09-16 04:56:42.604Z | 62.034° ENE |
| 8 mins | 2025-09-16 06:34:42.604Z | 324.146° NNW | 2025-09-16 06:37:42.604Z | 29.844° NE | 41.764° | 2025-09-16 06:42:42.604Z | 120.601° SE |
| 6 mins | 2025-09-16 08:18:42.604Z | 271.323° WNW | 2025-09-16 08:20:42.604Z | 241.447° WSW | 21.854° | 2025-09-16 08:24:42.604Z | 187.55° 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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