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, 1.0 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 S7
1 62576U 25007B 26315.57526748 -.00000110 00000-0 29210-4 0 9992
2 62576 54.9742 136.4999 0012617 8.1144 352.0014 13.80630659 95072Epoch: 2026-11-11T13:48Z
TLE epoch observation values (Epoch: 2026-11-11T13:48:23.110Z)
Latitude
-0.00001°
Longitude
-121.31755°
Altitude
953.501 km
Speed
7.381 km/s
True Right ascension
09h 05m 59s
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
19:48:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
970.881 km
Perigee altitude
952.359 km
Semi-major axis
7,339.757 km
Eccentricity
0.00126
Inclination
54.9742°
RAAN
136.4999°
Arg. of periapsis
8.1144°
True anomaly
351.98125°
Mean anomaly
352.0014°
Eccentric anomaly
351.99133°
Mean motion
3.4516 °/min
Orbital period
104.3 mins
BSTAR
0.00002921
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-11-12 14:17:06.837Z | 209.021° SW | 2026-11-12 14:22:06.837Z | 116.741° SE | 64° | 2026-11-12 14:28:06.837Z | 51.928° ENE |
| 10 mins | 2026-11-12 16:06:06.837Z | 270.079° WNW | 2026-11-12 16:11:06.837Z | 336.156° NNW | 36.527° | 2026-11-12 16:16:06.837Z | 35.175° NE |
| 7 mins | 2026-11-12 17:58:06.837Z | 319.535° NNW | 2026-11-12 18:01:06.837Z | 353.152° N | 20.568° | 2026-11-12 18:05:06.837Z | 36.548° NE |
| 9 mins | 2026-11-12 19:48:06.837Z | 332.964° NNW | 2026-11-12 19:52:06.837Z | 22.379° NNE | 27.027° | 2026-11-12 19:57:06.837Z | 75.815° E |
| 10 mins | 2026-11-12 21:37:06.837Z | 317.779° NNW | 2026-11-12 21:41:06.837Z | 2.479° NNE | 71.821° | 2026-11-12 21:47:06.837Z | 126.343° SE |
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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