CE-SAT IIB, 46818
Orbit data source: Space-Track
CE-SAT IIB, 46818 is a payload satellite owned by Canon STL (JP) in SSO that was launched on Wed, 28 Oct 2020 UTC via an ELECTRON launch vehicle from the Rocket Lab Launch Complex (RLLC). Payloads include a variety of satellites, spacecraft, and rockets 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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46818 intel report (Beta)
CE-SAT IIB details
| Identifier | |
| Orbit | SSO |
| Last TLE update | 8 hours ago |
| Origin | |
| Manufacturer | Canon STL |
| Mission | Operational Commercial Imaging |
| Bus & Motor | CE-SAT, Unknown motor |
| Mass | 35 kg wet, 35 kg dry |
| Launch date (UTC) | |
| Launch vehicle | |
| Launch site | |
| Object type | Payload Rocket body Debris |
| Shape & HBR | Box, Unknown HBR |
| Radar Cross Section | 0.575 m², Medium (>0.1 m² and < 1m²) |
Expand to show TLE details & history
TLE from 8 hours ago
0 CE-SAT IIB
1 46818U 20077F 24361.14706920 .00031558 00000-0 73172-3 0 9993
2 46818 97.2882 58.9275 0008072 20.2668 339.8899 15.42319165231194Epoch: 2024-12-26T03:31Z
Definitive object data (Epoch: 2024-12-26T03:31:46.778Z)
| Latitude | 0.00001° |
| Longitude | -89.14805° |
| Altitude | 437.222 km |
| Speed | 7.652 km/s |
| True Right ascension | 03h 55m 42s |
| True Declination | 0° 00' 00" |
| Sunlit | Object was in full shadow at TLE epoch |
Visualization TLE readout
| Latitude | 80.5389° |
| Longitude | 140.94108° |
| Altitude | 451.384 km |
| Speed | 7.649 km/s |
| Apparent Right ascension | 22h 26m 08s |
| Apparent Declination | 25° 19' 17" |
| Sunlit | Object is in daylight |
Visualization observer readout
| Local Sidereal Time | 11:05:11 |
| Azimuth | 9.667° NNE |
| Elevation | -24.131° |
| Doppler factor | 1 |
Orbital elements
| Apogee altitude | 441.698 km |
| Perigee altitude | 430.697 km |
| Semi-major axis | 6,814.335 km |
| Eccentricity | 0.0008072 |
| Inclination | 97.2882° |
| RAAN | 58.9275° |
| Arg. of periapsis | 20.2668° |
| True anomaly | 339.85807° |
| Mean anomaly | 339.8899° |
| Eccentric anomaly | 339.87399° |
| Mean motion | 3.85841 °/min |
| BSTAR | 0.00073172 |
| Orbital period | 93.3 mins |
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Other satellites on launch #77 in the year 2020 (2020-10-28 UTC)
CE-SAT IIB Visibility forecast
Observer location: undefined°, undefined
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 | 2024-12-26 16:32:47.547Z | 30.97° NE | 2024-12-26 16:35:47.547Z | 107.55° ESE | 30.853° | 2024-12-26 16:37:47.547Z | 160.112° S |
| 5 mins | 2024-12-27 04:34:47.547Z | 203.707° SW | 2024-12-27 04:36:47.547Z | 263.179° W | 30.082° | 2024-12-27 04:39:47.547Z | 330.101° NNW |
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