Spacecraft information: CE-SAT IIB
| Launched | 27 October 2020 |
| Flight ended | – |
| Status | Operational |
| Category |
Active satellites
|
| Launch site | |
| Owner | Japan |
| NORAD ID | 46818 |
| COSPAR ID | 2020-077F |
| Observing |
Current orbital elements
| Inclination | 97.231° |
| Eccentricity | 0.00051 |
| RA ascending node | 4.498 hr |
| Argument perigee | 100.666° |
| Mean anomaly | 259.518° |
| Orbital period | 91.709 min |
| Epoch of osculation | 24 Dec 2025, 07:09 |
Derived Quantities
| Min Altitude | 362.0 km |
| Mean Altitude | 365.5 km |
| Peak Altitude | 369.0 km |
Orbital History
Drag the graphs below left or right to change the time range, or use your scroll wheel to zoom in or out.