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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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: 7 hours ago
TLE from 7 hours ago
0 CENTISPACE-1 S9
1 62578U 25007D 26124.44629968 -.00000091 00000-0 47385-4 0 9997
2 62578 54.9816 85.2519 0011150 358.6189 1.4734 13.80590655 68679Epoch: 2026-05-04T10:42Z
TLE epoch observation values (Epoch: 2026-05-04T10:42:40.292Z)
Latitude
-0.00007°
Longitude
62.24859°
Altitude
954.633 km
Speed
7.379 km/s
True Right ascension
05h 41m 00s
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
01:38:51
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
969.945 km
Perigee altitude
953.577 km
Semi-major axis
7,339.898 km
Eccentricity
0.00112
Inclination
54.9816°
RAAN
85.2519°
Arg. of periapsis
358.6189°
True anomaly
1.47669°
Mean anomaly
1.4734°
Eccentric anomaly
1.47504°
Mean motion
3.4515 °/min
Orbital period
104.3 mins
BSTAR
0.000047385
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-05-04 22:59:49.705Z | 191.232° SSW | 2026-05-04 23:04:49.705Z | 133.693° SE | 32.09° | 2026-05-04 23:10:49.705Z | 60.629° ENE |
| 11 mins | 2026-05-05 00:48:49.705Z | 252.898° W | 2026-05-05 00:53:49.705Z | 327.742° NNW | 38.025° | 2026-05-05 00:59:49.705Z | 40.646° NE |
| 7 mins | 2026-05-05 02:40:49.705Z | 311.891° NW | 2026-05-05 02:43:49.705Z | 348.266° N | 21.088° | 2026-05-05 02:47:49.705Z | 32.485° NE |
| 8 mins | 2026-05-05 04:30:49.705Z | 330.326° NNW | 2026-05-05 04:34:49.705Z | 16.628° NNE | 21.041° | 2026-05-05 04:38:49.705Z | 59.214° ENE |
| 10 mins | 2026-05-05 06:19:49.705Z | 324.141° NNW | 2026-05-05 06:24:49.705Z | 43.648° NE | 37.858° | 2026-05-05 06:29:49.705Z | 108.045° ESE |
| 10 mins | 2026-05-05 08:08:49.705Z | 293.304° NW | 2026-05-05 08:12:49.705Z | 241.281° WSW | 32.442° | 2026-05-05 08:18:49.705Z | 167.196° S |
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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