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, Medium (>0.1 m² and < 1m²)
Expand to show TLE details & historyLast TLE update: 18 hours ago
TLE from 18 hours ago
0 CENTISPACE-1 S8
1 62577U 25007C 26135.27866684 -.00000070 00000-0 67312-4 0 9996
2 62577 54.9860 46.6484 0015808 60.2675 299.9852 13.80596933 70188Epoch: 2026-05-15T06:41Z
TLE epoch observation values (Epoch: 2026-05-15T06:41:16.814Z)
Latitude
-0.00005°
Longitude
73.31603°
Altitude
957.007 km
Speed
7.377 km/s
True Right ascension
03h 06m 35s
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
09:20:46
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
973.341 km
Perigee altitude
950.135 km
Semi-major axis
7,339.875 km
Eccentricity
0.00158
Inclination
54.986°
RAAN
46.6484°
Arg. of periapsis
60.2675°
True anomaly
299.82814°
Mean anomaly
299.9852°
Eccentric anomaly
299.90669°
Mean motion
3.45152 °/min
Orbital period
104.3 mins
BSTAR
0.000067312
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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 | 2026-05-16 02:16:14.044Z | 328.219° NNW | 2026-05-16 02:21:14.044Z | 33.355° NE | 28.438° | 2026-05-16 02:26:14.044Z | 88.216° E |
| 11 mins | 2026-05-16 04:05:14.044Z | 308.941° NW | 2026-05-16 04:10:14.044Z | 209.249° SW | 44.059° | 2026-05-16 04:16:14.044Z | 142.03° SSE |
| 4 mins | 2026-05-16 05:56:14.044Z | 259.076° W | 2026-05-16 05:58:14.044Z | 238.415° WSW | 13.852° | 2026-05-16 06:00:14.044Z | 218.611° SW |
| 9 mins | 2026-05-16 19:19:14.044Z | 180.158° SSW | 2026-05-16 19:23:14.044Z | 124.699° SE | 30.003° | 2026-05-16 19:28:14.044Z | 64.783° ENE |
| 10 mins | 2026-05-16 21:07:14.044Z | 251.152° W | 2026-05-16 21:11:14.044Z | 306.745° NW | 38.97° | 2026-05-16 21:17:14.044Z | 39.814° NE |
| 8 mins | 2026-05-16 22:58:14.044Z | 305.652° NW | 2026-05-16 23:01:14.044Z | 340.5° N | 21.313° | 2026-05-16 23:06:14.044Z | 35.553° NE |
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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