CENTISPACE-2 S2, 68351
Orbit data source: Space-Track
CENTISPACE-2 S2, 68351 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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68351 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, 0.9 m
Radar Cross Section
Large (>1 m²)
Expand to show TLE details & historyLast TLE update: 1 day ago
TLE from 1 day ago
0 CENTISPACE-2 S2
1 68351U 26060B 26170.81594552 .00000415 00000-0 11518-3 0 9991
2 68351 54.9820 26.8215 0006573 301.0410 58.9939 14.63748145 13131Epoch: 2026-06-19T19:34Z
TLE epoch observation values (Epoch: 2026-06-19T19:34:57.692Z)
Latitude
-0°
Longitude
-174.95838°
Altitude
679.771 km
Speed
7.519 km/s
True Right ascension
01h 47m 17s
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
07:21:43
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
685.704 km
Perigee altitude
676.424 km
Semi-major axis
7,059.201 km
Eccentricity
0.00066
Inclination
54.982°
RAAN
26.8215°
Arg. of periapsis
301.041°
True anomaly
59.05849°
Mean anomaly
58.9939°
Eccentric anomaly
59.02619°
Mean motion
3.6594 °/min
Orbital period
98.38 mins
BSTAR
0.00011518
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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 S2 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 22:15:57.243Z | 343.949° N | 2026-06-20 22:18:57.243Z | 31.023° NE | 19.993° | 2026-06-20 22:21:57.243Z | 70.937° E |
| 8 mins | 2026-06-20 23:57:57.243Z | 316.076° NNW | 2026-06-21 00:01:57.243Z | 104.13° ESE | 43.351° | 2026-06-21 00:05:57.243Z | 129.932° SE |
| 4 mins | 2026-06-21 01:41:57.243Z | 256.618° W | 2026-06-21 01:42:57.243Z | 242.529° WSW | 15.229° | 2026-06-21 01:45:57.243Z | 203.304° SW |
| 7 mins | 2026-06-21 15:59:57.243Z | 191.071° SSW | 2026-06-21 16:02:57.243Z | 119.147° SE | 35.051° | 2026-06-21 16:06:57.243Z | 59.471° ENE |
| 7 mins | 2026-06-21 17:41:57.243Z | 270.659° WNW | 2026-06-21 17:44:57.243Z | 324.181° NNW | 29.644° | 2026-06-21 17:48:57.243Z | 30.579° NE |
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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