CENTISPACE-1 S8, 62577
Orbit data source: Space-Track
CENTISPACE-1 S8, 62577 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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62577 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, 0.9 m
Radar Cross Section
0.833 m², Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 10 hours ago
TLE from 10 hours ago
0 CENTISPACE-1 S8
1 62577U 25007C 26202.17846533 -.00000101 00000-0 37342-4 0 9996
2 62577 54.9834 172.7135 0013680 181.5860 178.5055 13.80618367 79421Epoch: 2026-07-21T04:16Z
TLE epoch observation values (Epoch: 2026-07-21T04:16:59.404Z)
Latitude
-0.00003°
Longitude
169.51408°
Altitude
972.753 km
Speed
7.361 km/s
True Right ascension
11h 30m 51s
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
03:19:07
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
971.703 km
Perigee altitude
951.621 km
Semi-major axis
7,339.799 km
Eccentricity
0.00137
Inclination
54.9834°
RAAN
172.7135°
Arg. of periapsis
181.586°
True anomaly
178.50958°
Mean anomaly
178.5055°
Eccentric anomaly
178.50754°
Mean motion
3.45157 °/min
Orbital period
104.3 mins
BSTAR
0.000037342
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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 S8 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. |
|---|---|---|---|---|---|---|---|
| 10 mins | 2026-07-21 23:31:07.944Z | 186.846° SSW | 2026-07-21 23:36:07.944Z | 129.143° SE | 30.156° | 2026-07-21 23:41:07.944Z | 66.126° ENE |
| 10 mins | 2026-07-22 01:20:07.944Z | 250.081° W | 2026-07-22 01:25:07.944Z | 335.003° NNW | 39.427° | 2026-07-22 01:30:07.944Z | 39.062° NE |
| 8 mins | 2026-07-22 03:11:07.944Z | 303.473° NW | 2026-07-22 03:15:07.944Z | 350.759° N | 21.63° | 2026-07-22 03:19:07.944Z | 33.63° NE |
| 8 mins | 2026-07-22 05:02:07.944Z | 331.733° NNW | 2026-07-22 05:05:07.944Z | 5.535° NNE | 20.471° | 2026-07-22 05:10:07.944Z | 59.188° ENE |
| 10 mins | 2026-07-22 06:51:07.944Z | 326.168° NNW | 2026-07-22 06:56:07.944Z | 47.759° ENE | 35.951° | 2026-07-22 07:01:07.944Z | 105.528° ESE |
| 10 mins | 2026-07-22 08:40:07.944Z | 294.604° NW | 2026-07-22 08:44:07.944Z | 237.551° WSW | 34.611° | 2026-07-22 08:50:07.944Z | 162.967° 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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