CENTISPACE-2 S1, 68350
Orbit data source: Space-Track
CENTISPACE-2 S1, 68350 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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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, 1.0 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 S1
1 68350U 26060A 26170.92520555 .00000433 00000-0 11555-3 0 9995
2 68350 54.9822 26.1277 0007936 291.2890 68.7257 14.65045589 13157Epoch: 2026-06-19T22:12Z
TLE epoch observation values (Epoch: 2026-06-19T22:12:17.759Z)
Latitude
-0.00004°
Longitude
144.90648°
Altitude
675.964 km
Speed
7.521 km/s
True Right ascension
01h 44m 30s
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
08:41:36
Azimuth
Unknown
Elevation
Unknown
Doppler factor
Unknown
Orbital elements
Apogee altitude
682.494 km
Perigee altitude
671.297 km
Semi-major axis
7,055.032 km
Eccentricity
0.00079
Inclination
54.9822°
RAAN
26.1277°
Arg. of periapsis
291.289°
True anomaly
68.81047°
Mean anomaly
68.7257°
Eccentric anomaly
68.76808°
Mean motion
3.66264 °/min
Orbital period
98.29 mins
BSTAR
0.00011555
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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 S1 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. |
|---|---|---|---|---|---|---|---|
| 9 mins | 2026-06-20 23:14:37.566Z | 323.991° NNW | 2026-06-20 23:18:37.566Z | 19.307° NNE | 33.384° | 2026-06-20 23:23:37.566Z | 106.473° ESE |
| 6 mins | 2026-06-21 00:58:37.566Z | 283.231° WNW | 2026-06-21 01:01:37.566Z | 221.898° SW | 28.919° | 2026-06-21 01:04:37.566Z | 174.277° S |
| 5 mins | 2026-06-21 15:17:37.566Z | 157.563° S | 2026-06-21 15:19:37.566Z | 126.885° SE | 19.418° | 2026-06-21 15:22:37.566Z | 82.781° E |
| 7 mins | 2026-06-21 16:58:37.566Z | 243.538° WSW | 2026-06-21 17:01:37.566Z | 318.886° NNW | 41.905° | 2026-06-21 17:05:37.566Z | 40.083° NE |
| 5 mins | 2026-06-21 18:42:37.566Z | 309.169° NW | 2026-06-21 18:44:37.566Z | 339.194° N | 18.121° | 2026-06-21 18:47:37.566Z | 21.061° 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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