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: 17 hours ago
TLE from 17 hours ago
0 CENTISPACE-1 S9
1 62578U 25007D 26034.13712132 -.00000055 00000-0 64681-4 0 9997
2 62578 54.9828 43.2489 0008927 285.5950 74.4029 13.97964861 56164Epoch: 2026-02-03T03:17Z
TLE epoch observation values (Epoch: 2026-02-03T03:17:27.282Z)
Latitude
0.00002°
Longitude
-139.43713°
Altitude
900.139 km
Speed
7.404 km/s
True Right ascension
02h 52m 59s
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
21:58:48
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
907.317 km
Perigee altitude
894.321 km
Semi-major axis
7,278.956 km
Eccentricity
0.00089
Inclination
54.9828°
RAAN
43.2489°
Arg. of periapsis
285.595°
True anomaly
74.50146°
Mean anomaly
74.4029°
Eccentric anomaly
74.45218°
Mean motion
3.49494 °/min
Orbital period
103.01 mins
BSTAR
0.000064681
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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 | 2026-02-04 01:43:13.764Z | 179.68° S | 2026-02-04 01:48:13.764Z | 119.406° SE | 25.633° | 2026-02-04 01:52:13.764Z | 71.441° E |
| 10 mins | 2026-02-04 03:30:13.764Z | 243.361° WSW | 2026-02-04 03:35:13.764Z | 336.547° NNW | 41.331° | 2026-02-04 03:40:13.764Z | 41.043° NE |
| 7 mins | 2026-02-04 05:20:13.764Z | 303.927° NW | 2026-02-04 05:23:13.764Z | 341.873° N | 21.796° | 2026-02-04 05:27:13.764Z | 29.336° NE |
| 6 mins | 2026-02-04 07:10:13.764Z | 338.909° N | 2026-02-04 07:12:13.764Z | 2.948° NNE | 18.672° | 2026-02-04 07:16:13.764Z | 48.3° ENE |
| 9 mins | 2026-02-04 08:57:13.764Z | 329.502° NNW | 2026-02-04 09:01:13.764Z | 26.06° NE | 32.171° | 2026-02-04 09:06:13.764Z | 95.353° ESE |
| 10 mins | 2026-02-04 10:44:13.764Z | 302.298° NW | 2026-02-04 10:49:13.764Z | 218.461° SW | 39.154° | 2026-02-04 10:54:13.764Z | 155.101° SSE |
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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