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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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: 3 days ago
TLE from 3 days ago
0 CENTISPACE-1 S8
1 62577U 25007C 25255.91017159 -.00000065 00000-0 29570-4 0 9992
2 62577 54.9839 224.0262 0070117 350.0050 9.9538 14.47490177 35729Epoch: 2025-09-12T21:50Z
TLE epoch observation values (Epoch: 2025-09-12T21:50:38.825Z)
Latitude
-0.00003°
Longitude
-95.7867°
Altitude
685.806 km
Speed
7.54 km/s
True Right ascension
14h 56m 06s
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
03:05:59
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
783.691 km
Perigee altitude
683.957 km
Semi-major axis
7,111.961 km
Eccentricity
0.00701
Inclination
54.9839°
RAAN
224.0262°
Arg. of periapsis
350.005°
True anomaly
10.09389°
Mean anomaly
9.9538°
Eccentric anomaly
10.02373°
Mean motion
3.61875 °/min
Orbital period
99.48 mins
BSTAR
0.00002957
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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. |
|---|---|---|---|---|---|---|---|
| 8 mins | 2025-09-15 22:53:53.774Z | 192.332° SSW | 2025-09-15 22:57:53.774Z | 136.946° SSE | 29.84° | 2025-09-15 23:01:53.774Z | 67.436° ENE |
| 7 mins | 2025-09-16 00:38:53.774Z | 266.557° W | 2025-09-16 00:41:53.774Z | 333.626° NNW | 33.73° | 2025-09-16 00:45:53.774Z | 34.514° NE |
| 4 mins | 2025-09-16 02:24:53.774Z | 327.09° NNW | 2025-09-16 02:25:53.774Z | 340.907° N | 16.049° | 2025-09-16 02:28:53.774Z | 20.462° NNE |
| 5 mins | 2025-09-16 04:09:53.774Z | 347.317° N | 2025-09-16 04:11:53.774Z | 14.136° NNE | 15.844° | 2025-09-16 04:14:53.774Z | 49.678° ENE |
| 8 mins | 2025-09-16 05:52:53.774Z | 331.669° NNW | 2025-09-16 05:56:53.774Z | 44.103° NE | 31.459° | 2025-09-16 06:00:53.774Z | 98.6° ESE |
| 8 mins | 2025-09-16 07:36:53.774Z | 293.134° NW | 2025-09-16 07:39:53.774Z | 237.393° WSW | 35.629° | 2025-09-16 07:44:53.774Z | 159.551° S |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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