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: 16 hours ago
TLE from 16 hours ago
0 CENTISPACE-1 S15
1 62584U 25007K 26034.08356323 .00000020 00000-0 11616-3 0 9994
2 62584 54.9936 43.6967 0011109 261.4981 98.4724 13.98319492 56173Epoch: 2026-02-03T02:00Z
TLE epoch observation values (Epoch: 2026-02-03T02:00:19.863Z)
Latitude
-0.00005°
Longitude
-119.65569°
Altitude
901.851 km
Speed
7.401 km/s
True Right ascension
02h 54m 47s
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
20:14:20
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
907.671 km
Perigee altitude
891.501 km
Semi-major axis
7,277.723 km
Eccentricity
0.00111
Inclination
54.9936°
RAAN
43.6967°
Arg. of periapsis
261.4981°
True anomaly
98.59828°
Mean anomaly
98.4724°
Eccentric anomaly
98.53534°
Mean motion
3.49583 °/min
Orbital period
102.98 mins
BSTAR
0.00011616
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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 | 2026-02-04 02:09:03.022Z | 195.594° SSW | 2026-02-04 02:14:03.022Z | 133.906° SE | 34.129° | 2026-02-04 02:19:03.022Z | 62.125° ENE |
| 10 mins | 2026-02-04 03:57:03.022Z | 258.144° W | 2026-02-04 04:02:03.022Z | 340.547° N | 35.411° | 2026-02-04 04:07:03.022Z | 38.307° NE |
| 7 mins | 2026-02-04 05:47:03.022Z | 311.321° NW | 2026-02-04 05:50:03.022Z | 346.65° N | 19.628° | 2026-02-04 05:54:03.022Z | 31.992° NE |
| 7 mins | 2026-02-04 07:36:03.022Z | 332.811° NNW | 2026-02-04 07:39:03.022Z | 7.397° NNE | 20.163° | 2026-02-04 07:43:03.022Z | 55.128° ENE |
| 9 mins | 2026-02-04 09:24:03.022Z | 327.122° NNW | 2026-02-04 09:28:03.022Z | 36.618° NE | 37.932° | 2026-02-04 09:33:03.022Z | 108.752° ESE |
| 9 mins | 2026-02-04 11:11:03.022Z | 291.944° WNW | 2026-02-04 11:15:03.022Z | 236.392° WSW | 31.175° | 2026-02-04 11:20:03.022Z | 170.866° 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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