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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Edit Public Description
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: 15 hours ago
TLE from 15 hours ago
0 CENTISPACE-1 S15
1 62584U 25007K 25319.71376139 .00000703 00000-0 31691-3 0 9999
2 62584 54.9838 337.3280 0008027 281.9713 78.0367 14.32471683 44949Epoch: 2025-11-15T17:07Z
TLE epoch observation values (Epoch: 2025-11-15T17:07:48.984Z)
Latitude
-0.00001°
Longitude
25.33494°
Altitude
783.341 km
Speed
7.464 km/s
True Right ascension
22h 29m 18s
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
04:33:10
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
789.196 km
Perigee altitude
777.699 km
Semi-major axis
7,161.585 km
Eccentricity
0.0008
Inclination
54.9838°
RAAN
337.328°
Arg. of periapsis
281.9713°
True anomaly
78.1267°
Mean anomaly
78.0367°
Eccentric anomaly
78.0817°
Mean motion
3.58121 °/min
Orbital period
100.52 mins
BSTAR
0.00031691
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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. |
|---|---|---|---|---|---|---|---|
| 7 mins | 2025-11-16 08:37:04.116Z | 329.71° NNW | 2025-11-16 08:41:04.116Z | 17.623° NNE | 18.005° | 2025-11-16 08:44:04.116Z | 54.108° ENE |
| 8 mins | 2025-11-16 10:23:04.116Z | 328.738° NNW | 2025-11-16 10:27:04.116Z | 51.616° ENE | 36.193° | 2025-11-16 10:31:04.116Z | 107.353° ESE |
| 7 mins | 2025-11-16 12:08:04.116Z | 285.058° WNW | 2025-11-16 12:11:04.116Z | 234.655° WSW | 29.565° | 2025-11-16 12:15:04.116Z | 174.492° S |
| 8 mins | 2025-11-17 02:46:04.116Z | 186.887° SSW | 2025-11-17 02:50:04.116Z | 121.944° SE | 30.856° | 2025-11-17 02:54:04.116Z | 65.379° ENE |
| 8 mins | 2025-11-17 04:31:04.116Z | 261.103° W | 2025-11-17 04:34:04.116Z | 313.608° NW | 35.373° | 2025-11-17 04:39:04.116Z | 36.279° NE |
| 5 mins | 2025-11-17 06:18:04.116Z | 317.952° NNW | 2025-11-17 06:20:04.116Z | 344.221° N | 17.696° | 2025-11-17 06:23:04.116Z | 22.413° NNE |
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 ascending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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