View from above orbital plane
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View from above satellite
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Ground track
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The orbit data is extracted from the following two-line orbital elements,
1 45117U 19071G 23040.94526179 .13206057 12424-4 72377-3 0 9998
2 45117 51.6075 295.4096 0005383 247.2408 112.8051 16.42175522170567
Epoch (UTC): | 09 February 2023 22:41:10 |
Eccentricity: | 0.0005383 |
inclination: | 51.6075° |
perigee height: | 156 km |
apogee height: | 163 km |
right ascension of ascending node: | 295.4096° |
argument of perigee: | 247.2408° |
revolutions per day: | 16.42175522 |
mean anomaly at epoch: | 112.8051° |
orbit number at epoch: | 17056 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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