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: 7 hours ago
TLE from 7 hours ago
0 CENTISPACE-1 S7
1 62576U 25007B 26262.43201422 -.00000066 00000-0 70116-4 0 9998
2 62576 54.9778 322.3742 0010678 247.2533 112.7295 13.80623542 87735Epoch: 2026-09-19T10:22Z
TLE epoch observation values (Epoch: 2026-09-19T10:22:06.028Z)
Latitude
-0.00003°
Longitude
168.50842°
Altitude
965.732 km
Speed
7.368 km/s
True Right ascension
21h 29m 29s
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
10:04:49
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
969.482 km
Perigee altitude
953.807 km
Semi-major axis
7,339.782 km
Eccentricity
0.00107
Inclination
54.9778°
RAAN
322.3742°
Arg. of periapsis
247.2533°
True anomaly
112.8423°
Mean anomaly
112.7295°
Eccentric anomaly
112.78591°
Mean motion
3.45158 °/min
Orbital period
104.3 mins
BSTAR
0.000070116
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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 | 2026-09-20 05:35:49.134Z | 191.356° SSW | 2026-09-20 05:41:49.134Z | 119.765° SE | 37.891° | 2026-09-20 05:46:49.134Z | 62.765° ENE |
| 10 mins | 2026-09-20 07:25:49.134Z | 254.393° W | 2026-09-20 07:29:49.134Z | 314.781° NW | 52.841° | 2026-09-20 07:35:49.134Z | 39.623° NE |
| 8 mins | 2026-09-20 09:16:49.134Z | 307.986° NW | 2026-09-20 09:19:49.134Z | 342.764° N | 23.111° | 2026-09-20 09:24:49.134Z | 36.376° NE |
| 8 mins | 2026-09-20 11:07:49.134Z | 335.529° NNW | 2026-09-20 11:10:49.134Z | 10.869° NNE | 22.577° | 2026-09-20 11:15:49.134Z | 62.328° ENE |
| 11 mins | 2026-09-20 12:55:49.134Z | 323.032° NNW | 2026-09-20 13:00:49.134Z | 29.736° NE | 49.554° | 2026-09-20 13:06:49.134Z | 108.445° ESE |
| 10 mins | 2026-09-20 14:44:49.134Z | 296.607° NW | 2026-09-20 14:49:49.134Z | 228.365° WSW | 41.606° | 2026-09-20 14:54:49.134Z | 167.389° 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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