CENTISPACE-2 S9, 68358
Orbit data source: Space-Track
CENTISPACE-2 S9, 68358 is a payload satellite owned by Centispace (CN) in LEO that was launched on Sun, 22 Mar 2026 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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68358 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
HITSAT
Mission
Operational spacecraft
Bus & Motor
WK01H, Unknown motor
Mass
140 kg wet, 140 kg dry
Launch date (UTC)
Launch vehicle
Launch site
Object type
Shape & HBR
Unknown shape, 1.1 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 22 hours ago
TLE from 22 hours ago
0 CENTISPACE-2 S9
1 68358U 26060J 26170.93010283 .00000518 00000-0 13425-3 0 9998
2 68358 54.9818 26.1487 0013538 305.3819 54.5910 14.63992286 13158Epoch: 2026-06-19T22:19Z
TLE epoch observation values (Epoch: 2026-06-19T22:19:20.884Z)
Latitude
-0.00002°
Longitude
143.15965°
Altitude
675.846 km
Speed
7.523 km/s
True Right ascension
01h 44m 35s
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
07:20:15
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
689.835 km
Perigee altitude
670.723 km
Semi-major axis
7,058.416 km
Eccentricity
0.00135
Inclination
54.9818°
RAAN
26.1487°
Arg. of periapsis
305.3819°
True anomaly
54.71756°
Mean anomaly
54.591°
Eccentric anomaly
54.65427°
Mean motion
3.66001 °/min
Orbital period
98.36 mins
BSTAR
0.00013425
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Other satellites on launch #60 in the year 2026 (2026-03-22 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-2 S9 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. |
|---|---|---|---|---|---|---|---|
| 5 mins | 2026-06-20 21:41:29.439Z | 339.076° N | 2026-06-20 21:44:29.439Z | 19.409° NNE | 16.242° | 2026-06-20 21:46:29.439Z | 46.777° ENE |
| 7 mins | 2026-06-20 23:24:29.439Z | 329.891° NNW | 2026-06-20 23:27:29.439Z | 32.535° NE | 36.605° | 2026-06-20 23:31:29.439Z | 108.108° ESE |
| 6 mins | 2026-06-21 01:07:29.439Z | 275.626° WNW | 2026-06-21 01:09:29.439Z | 238.906° WSW | 26.141° | 2026-06-21 01:13:29.439Z | 176.726° S |
| 6 mins | 2026-06-21 15:26:29.439Z | 165.009° S | 2026-06-21 15:28:29.439Z | 133.054° SE | 22.286° | 2026-06-21 15:32:29.439Z | 73.597° E |
| 8 mins | 2026-06-21 17:07:29.439Z | 248.143° W | 2026-06-21 17:10:29.439Z | 300.132° NW | 38.721° | 2026-06-21 17:15:29.439Z | 39.654° NE |
| 4 mins | 2026-06-21 18:52:29.439Z | 317.562° NNW | 2026-06-21 18:54:29.439Z | 347.754° N | 17.071° | 2026-06-21 18:56:29.439Z | 15.514° 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 descending order |
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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