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 51U 60009C 23343.49873690 .00000022 00000-0 10349-2 0 9995
2 51 47.2152 18.1565 0107797 337.7851 21.8288 12.18311822818915
Epoch (UTC): | 09 December 2023 11:58:10 |
Eccentricity: | 0.0107797 |
inclination: | 47.2152° |
perigee height: | 1514 km |
apogee height: | 1686 km |
right ascension of ascending node: | 18.1565° |
argument of perigee: | 337.7851° |
revolutions per day: | 12.18311822 |
mean anomaly at epoch: | 21.8288° |
orbit number at epoch: | 81891 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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