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: 7 hours ago
TLE from 7 hours ago
0 CENTISPACE-1 S15
1 62584U 25007K 26124.46070057 -.00000011 00000-0 12298-3 0 9991
2 62584 54.9857 85.4623 0013121 356.8042 3.2828 13.80609609 68693Epoch: 2026-05-04T11:03Z
TLE epoch observation values (Epoch: 2026-05-04T11:03:24.529Z)
Latitude
-0.00005°
Longitude
57.26049°
Altitude
953.132 km
Speed
7.381 km/s
True Right ascension
05h 41m 50s
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
01:38:14
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
971.323 km
Perigee altitude
952.062 km
Semi-major axis
7,339.83 km
Eccentricity
0.00131
Inclination
54.9857°
RAAN
85.4623°
Arg. of periapsis
356.8042°
True anomaly
3.29142°
Mean anomaly
3.2828°
Eccentric anomaly
3.28711°
Mean motion
3.45155 °/min
Orbital period
104.3 mins
BSTAR
0.00012298
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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. |
|---|---|---|---|---|---|---|---|
| 11 mins | 2026-05-04 23:21:12.550Z | 202.608° SW | 2026-05-04 23:26:12.550Z | 142.383° SSE | 38.329° | 2026-05-04 23:32:12.550Z | 56.222° ENE |
| 10 mins | 2026-05-05 01:11:12.550Z | 266.715° W | 2026-05-05 01:15:12.550Z | 323.021° NNW | 33.514° | 2026-05-05 01:21:12.550Z | 38.191° NE |
| 8 mins | 2026-05-05 03:02:12.550Z | 312.942° NW | 2026-05-05 03:05:12.550Z | 345.744° N | 19.714° | 2026-05-05 03:10:12.550Z | 39.027° NE |
| 8 mins | 2026-05-05 04:53:12.550Z | 337.028° NNW | 2026-05-05 04:56:12.550Z | 13.879° NNE | 22.892° | 2026-05-05 05:01:12.550Z | 69.025° E |
| 11 mins | 2026-05-05 06:41:12.550Z | 319.618° NNW | 2026-05-05 06:46:12.550Z | 38.405° NE | 42.137° | 2026-05-05 06:52:12.550Z | 120.196° SE |
| 8 mins | 2026-05-05 08:31:12.550Z | 280.672° WNW | 2026-05-05 08:34:12.550Z | 242.207° WSW | 25.972° | 2026-05-05 08:39:12.550Z | 182.639° SSW |
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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