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CE-SAT IIB
Launch Details
| Launched | 27 October 2020 |
| Flight ended | – |
| Status | Operational |
| Launch site | |
| Owner | Japan |
| NORAD ID | 46818 |
| COSPAR ID | 2020-077F |
| Observing |
Current orbital elements
| Inclination | 97.368° |
| Eccentricity | 0.00108 |
| RA ascending node | 14.127 hr |
| Argument perihelion | 252.208° |
| Mean anomaly | 107.798° |
| Orbital period | 94.562 min |
| Epoch of osculation | 31 May 2023, 09:25 |
Derived Quantities
| Min Altitude | 497.1 km |
| Mean Altitude | 504.5 km |
| Peak Altitude | 512.0 km |
Orbital History
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