CENTISPACE-2 S8, 68357
Orbit data source: Space-Track
CENTISPACE-2 S8, 68357 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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68357 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: 13 hours ago
TLE from 13 hours ago
0 CENTISPACE-2 S8
1 68357U 26060H 26171.31314565 .00000544 00000-0 13592-3 0 9994
2 68357 54.9863 24.4032 0012045 307.6046 52.3855 14.65174012 13215Epoch: 2026-06-20T07:30Z
TLE epoch observation values (Epoch: 2026-06-20T07:30:55.784Z)
Latitude
0.00001°
Longitude
3.14121°
Altitude
672.4 km
Speed
7.524 km/s
True Right ascension
01h 37m 36s
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
07:21:52
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
684.98 km
Perigee altitude
667.985 km
Semi-major axis
7,054.62 km
Eccentricity
0.0012
Inclination
54.9863°
RAAN
24.4032°
Arg. of periapsis
307.6046°
True anomaly
52.49494°
Mean anomaly
52.3855°
Eccentric anomaly
52.44021°
Mean motion
3.66297 °/min
Orbital period
98.28 mins
BSTAR
0.00013592
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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 S8 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. |
|---|---|---|---|---|---|---|---|
| 4 mins | 2026-06-20 21:01:06.440Z | 341.52° N | 2026-06-20 21:03:06.440Z | 7.473° NNE | 13.585° | 2026-06-20 21:05:06.440Z | 33.194° NE |
| 6 mins | 2026-06-20 22:44:06.440Z | 342.678° N | 2026-06-20 22:47:06.440Z | 38.235° NE | 25.451° | 2026-06-20 22:50:06.440Z | 83.357° E |
| 7 mins | 2026-06-21 00:26:06.440Z | 301.894° NW | 2026-06-21 00:29:06.440Z | 234.784° WSW | 41.257° | 2026-06-21 00:33:06.440Z | 149.968° SSE |
| 8 mins | 2026-06-21 16:26:06.440Z | 217.607° SW | 2026-06-21 16:29:06.440Z | 169.42° S | 43.804° | 2026-06-21 16:34:06.440Z | 49.818° ENE |
| 6 mins | 2026-06-21 18:09:06.440Z | 286.784° WNW | 2026-06-21 18:12:06.440Z | 335.109° NNW | 23.07° | 2026-06-21 18:15:06.440Z | 21.751° NNE |
Co-orbital & Co-planar RSOs
Thresholds — Semi-major Axis: ±100 km, RAAN: ±3°, Inclination: ±5°
TCA is derived from TLE conjunctions
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CAUTION: Conjunctions in this section are generated from low-fidelity TLE screenings
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