CENTISPACE-1 S11, 62580
Orbit data source: Space-Track
CENTISPACE-1 S11, 62580 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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62580 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: 9 hours ago
TLE from 9 hours ago
0 CENTISPACE-1 S11
1 62580U 25007F 26202.24350426 -.00000074 00000-0 63135-4 0 9997
2 62580 54.9760 171.9977 0011277 154.6688 205.4823 13.80617371 79435Epoch: 2026-07-21T05:50Z
TLE epoch observation values (Epoch: 2026-07-21T05:50:38.768Z)
Latitude
-0.00001°
Longitude
145.32017°
Altitude
970.192 km
Speed
7.364 km/s
True Right ascension
11h 27m 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
03:21:06
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
969.944 km
Perigee altitude
953.39 km
Semi-major axis
7,339.804 km
Eccentricity
0.00113
Inclination
54.976°
RAAN
171.9977°
Arg. of periapsis
154.6688°
True anomaly
205.42677°
Mean anomaly
205.4823°
Eccentric anomaly
205.45453°
Mean motion
3.45157 °/min
Orbital period
104.3 mins
BSTAR
0.000063135
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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 S11 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 | 2026-07-21 23:20:06.666Z | 182.85° SSW | 2026-07-21 23:25:06.666Z | 129.365° SE | 27.13° | 2026-07-21 23:30:06.666Z | 68.833° E |
| 10 mins | 2026-07-22 01:09:06.666Z | 244.996° WSW | 2026-07-22 01:14:06.666Z | 336.667° NNW | 41.192° | 2026-07-22 01:19:06.666Z | 40.525° NE |
| 8 mins | 2026-07-22 03:00:06.666Z | 301.546° NW | 2026-07-22 03:04:06.666Z | 350.735° N | 22.307° | 2026-07-22 03:08:06.666Z | 33.477° NE |
| 7 mins | 2026-07-22 04:51:06.666Z | 331.475° NNW | 2026-07-22 04:54:06.666Z | 5.517° NNE | 19.966° | 2026-07-22 04:58:06.666Z | 50.344° ENE |
| 10 mins | 2026-07-22 06:40:06.666Z | 327.533° NNW | 2026-07-22 06:44:06.666Z | 20.525° NNE | 34.071° | 2026-07-22 06:50:06.666Z | 101.566° ESE |
| 10 mins | 2026-07-22 08:29:06.666Z | 297.821° NW | 2026-07-22 08:33:06.666Z | 239.343° WSW | 37.325° | 2026-07-22 08:39:06.666Z | 158.423° 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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