CENTISPACE-1 S7, 62576
Orbit data source: Space-Track
CENTISPACE-1 S7, 62576 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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62576 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 S7
1 62576U 25007B 26135.29252099 -.00000070 00000-0 67329-4 0 9994
2 62576 54.9774 47.0409 0012753 9.7885 350.3318 13.80590601 70174Epoch: 2026-05-15T07:01Z
TLE epoch observation values (Epoch: 2026-05-15T07:01:13.813Z)
Latitude
0.00003°
Longitude
68.70744°
Altitude
953.586 km
Speed
7.381 km/s
True Right ascension
03h 08m 09s
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
09:20:13
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
971.122 km
Perigee altitude
952.401 km
Semi-major axis
7,339.898 km
Eccentricity
0.00128
Inclination
54.9774°
RAAN
47.0409°
Arg. of periapsis
9.7885°
True anomaly
350.30722°
Mean anomaly
350.3318°
Eccentric anomaly
350.31951°
Mean motion
3.4515 °/min
Orbital period
104.3 mins
BSTAR
0.000067329
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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 S7 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 | 2026-05-16 00:47:40.452Z | 324.818° NNW | 2026-05-16 00:51:40.452Z | 8.754° NNE | 19.588° | 2026-05-16 00:55:40.452Z | 50.686° ENE |
| 10 mins | 2026-05-16 02:37:40.452Z | 330.492° NNW | 2026-05-16 02:41:40.452Z | 26.76° NE | 32.305° | 2026-05-16 02:47:40.452Z | 98.12° ESE |
| 11 mins | 2026-05-16 04:25:40.452Z | 304.029° NW | 2026-05-16 04:30:40.452Z | 234.034° WSW | 40.47° | 2026-05-16 04:36:40.452Z | 152.498° SSE |
| 10 mins | 2026-05-16 19:39:40.452Z | 192.598° SSW | 2026-05-16 19:43:40.452Z | 131.712° SE | 36.114° | 2026-05-16 19:49:40.452Z | 57.335° ENE |
| 10 mins | 2026-05-16 21:27:40.452Z | 259.273° W | 2026-05-16 21:32:40.452Z | 330.661° NNW | 35.299° | 2026-05-16 21:37:40.452Z | 36.198° NE |
| 7 mins | 2026-05-16 23:19:40.452Z | 314.614° NW | 2026-05-16 23:22:40.452Z | 349.776° N | 20.251° | 2026-05-16 23:26:40.452Z | 33.697° 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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