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 23332.58925968 -.00000026 00000-0 56263-3 0 9990
2 51 47.2151 51.9079 0107388 305.4601 53.6202 12.18311115817586
Epoch (UTC): | 28 November 2023 14:08:32 |
Eccentricity: | 0.0107388 |
inclination: | 47.2151° |
perigee height: | 1514 km |
apogee height: | 1685 km |
right ascension of ascending node: | 51.9079° |
argument of perigee: | 305.4601° |
revolutions per day: | 12.18311115 |
mean anomaly at epoch: | 53.6202° |
orbit number at epoch: | 81758 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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