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: 5 hours ago
TLE from 5 hours ago
0 CENTISPACE-1 S15
1 62584U 25007K 26137.20366076 -.00000044 00000-0 91921-4 0 9993
2 62584 54.9877 40.9059 0014050 22.0371 338.1186 13.80612205 70453Epoch: 2026-05-17T04:53Z
TLE epoch observation values (Epoch: 2026-05-17T04:53:16.289Z)
Latitude
-0.00009°
Longitude
92.67833°
Altitude
953.171 km
Speed
7.381 km/s
True Right ascension
02h 43m 37s
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
18:16:58
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
971.996 km
Perigee altitude
951.371 km
Semi-major axis
7,339.82 km
Eccentricity
0.00141
Inclination
54.9877°
RAAN
40.9059°
Arg. of periapsis
22.0371°
True anomaly
338.0585°
Mean anomaly
338.1186°
Eccentric anomaly
338.08856°
Mean motion
3.45156 °/min
Orbital period
104.3 mins
BSTAR
0.000091921
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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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-05-17 18:55:01.598Z | 177.763° S | 2026-05-17 18:59:01.598Z | 131.385° SE | 26.618° | 2026-05-17 19:04:01.598Z | 69.585° E |
| 11 mins | 2026-05-17 20:43:01.598Z | 244.308° WSW | 2026-05-17 20:48:01.598Z | 332.041° NNW | 41.359° | 2026-05-17 20:54:01.598Z | 42.629° NE |
| 8 mins | 2026-05-17 22:34:01.598Z | 300.6° NW | 2026-05-17 22:38:01.598Z | 349.426° N | 22.314° | 2026-05-17 22:42:01.598Z | 32.833° NE |
| 8 mins | 2026-05-18 00:25:01.598Z | 330.691° NNW | 2026-05-18 00:28:01.598Z | 4.349° NNE | 19.907° | 2026-05-18 00:33:01.598Z | 56.824° ENE |
| 10 mins | 2026-05-18 02:14:01.598Z | 327.16° NNW | 2026-05-18 02:19:01.598Z | 43.163° NE | 34.03° | 2026-05-18 02:24:01.598Z | 100.827° ESE |
| 10 mins | 2026-05-18 04:03:01.598Z | 298.538° NW | 2026-05-18 04:07:01.598Z | 242.926° WSW | 37.506° | 2026-05-18 04:13:01.598Z | 158.477° 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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