CENTISPACE-1 S15, 62584
Orbit data source: Space-Track
CENTISPACE-1 S15, 62584 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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62584 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
HITSAT
Mission
Operational Commercial Nav/Com
Bus & Motor
WK01H, 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: 6 hours ago
TLE from 6 hours ago
0 CENTISPACE-1 S15
1 62584U 25007K 26047.12180630 -.00000002 00000-0 10912-3 0 9998
2 62584 54.9883 356.9698 0009937 270.5302 89.4522 13.93306815 57996Epoch: 2026-02-16T02:55Z
TLE epoch observation values (Epoch: 2026-02-16T02:55:24.064Z)
Latitude
0.00003°
Longitude
166.99886°
Altitude
918.031 km
Speed
7.394 km/s
True Right ascension
23h 47m 52s
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
11:55:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
924.281 km
Perigee altitude
909.783 km
Semi-major axis
7,295.169 km
Eccentricity
0.00099
Inclination
54.9883°
RAAN
356.9698°
Arg. of periapsis
270.5302°
True anomaly
89.56607°
Mean anomaly
89.4522°
Eccentric anomaly
89.50913°
Mean motion
3.48329 °/min
Orbital period
103.35 mins
BSTAR
0.00010912
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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 S15 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 | 2026-02-16 21:58:56.503Z | 186.937° SSW | 2026-02-16 22:03:56.503Z | 129.145° SE | 29.202° | 2026-02-16 22:08:56.503Z | 65.993° ENE |
| 10 mins | 2026-02-16 23:46:56.503Z | 249.297° W | 2026-02-16 23:51:56.503Z | 336.69° NNW | 39.278° | 2026-02-16 23:56:56.503Z | 39.524° NE |
| 8 mins | 2026-02-17 01:36:56.503Z | 303.388° NW | 2026-02-17 01:40:56.503Z | 351.881° N | 20.981° | 2026-02-17 01:44:56.503Z | 34.339° NE |
| 7 mins | 2026-02-17 03:26:56.503Z | 332.487° NNW | 2026-02-17 03:29:56.503Z | 7.066° NNE | 19.606° | 2026-02-17 03:33:56.503Z | 52.307° ENE |
| 10 mins | 2026-02-17 05:14:56.503Z | 327.526° NNW | 2026-02-17 05:18:56.503Z | 23.716° NE | 34.736° | 2026-02-17 05:24:56.503Z | 104.178° ESE |
| 9 mins | 2026-02-17 07:02:56.503Z | 295.831° NW | 2026-02-17 07:06:56.503Z | 233.801° WSW | 35.981° | 2026-02-17 07:11:56.503Z | 163.029° 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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