CENTISPACE-2 S6, 68355
Orbit data source: Space-Track
CENTISPACE-2 S6, 68355 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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68355 intel report (Beta)
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Identifier
Orbit
Country
CN / PRCRelated business
Manufacturer
DFH Shenzhen
Mission
Operational spacecraft
Bus & Motor
WK01, 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 S6
1 68355U 26060F 26170.92957089 .00000515 00000-0 13360-3 0 9993
2 68355 54.9769 26.1024 0015852 306.5909 53.3626 14.64009357 13151Epoch: 2026-06-19T22:18Z
TLE epoch observation values (Epoch: 2026-06-19T22:18:34.924Z)
Latitude
-0.00006°
Longitude
143.30534°
Altitude
674.654 km
Speed
7.524 km/s
True Right ascension
01h 44m 24s
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
07:19:18
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
691.414 km
Perigee altitude
669.036 km
Semi-major axis
7,058.362 km
Eccentricity
0.00159
Inclination
54.9769°
RAAN
26.1024°
Arg. of periapsis
306.5909°
True anomaly
53.50853°
Mean anomaly
53.3626°
Eccentric anomaly
53.43555°
Mean motion
3.66005 °/min
Orbital period
98.36 mins
BSTAR
0.0001336
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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 S6 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. |
|---|---|---|---|---|---|---|---|
| 6 mins | 2026-06-20 21:40:32.633Z | 337.666° N | 2026-06-20 21:43:32.633Z | 17.262° NNE | 16.264° | 2026-06-20 21:46:32.633Z | 55.677° ENE |
| 7 mins | 2026-06-20 23:23:32.633Z | 329.086° NNW | 2026-06-20 23:26:32.633Z | 26.827° NE | 36.299° | 2026-06-20 23:30:32.633Z | 107.038° ESE |
| 6 mins | 2026-06-21 01:06:32.633Z | 277.639° WNW | 2026-06-21 01:08:32.633Z | 242.262° WSW | 26.241° | 2026-06-21 01:12:32.633Z | 177.45° S |
| 6 mins | 2026-06-21 15:25:32.633Z | 166.154° S | 2026-06-21 15:28:32.633Z | 115.861° SE | 22.009° | 2026-06-21 15:31:32.633Z | 74.817° E |
| 8 mins | 2026-06-21 17:06:32.633Z | 247.119° WSW | 2026-06-21 17:10:32.633Z | 345.293° N | 38.774° | 2026-06-21 17:14:32.633Z | 39.423° NE |
| 5 mins | 2026-06-21 18:51:32.633Z | 315.851° NNW | 2026-06-21 18:53:32.633Z | 345.832° N | 17.225° | 2026-06-21 18:56:32.633Z | 24.591° NE |
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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