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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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