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 22138.42194376 .00042645 00000-0 85735-3 0 9990
2 45117 51.6366 202.5849 0009095 50.3298 309.8490 15.46159560128788
Epoch (UTC): | 18 May 2022 10:07:35 |
Eccentricity: | 0.0009095 |
inclination: | 51.6366° |
perigee height: | 422 km |
apogee height: | 434 km |
right ascension of ascending node: | 202.5849° |
argument of perigee: | 50.3298° |
revolutions per day: | 15.46159560 |
mean anomaly at epoch: | 309.8490° |
orbit number at epoch: | 12878 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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