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 00051U 60009C 24306.67741476 .00000061 00000-0 14058-2 0 9995
2 00051 47.2130 82.7516 0107152 233.7443 125.3405 12.18341729858937
Epoch (UTC): | 01 November 2024 16:15:28 |
Eccentricity: | 0.0107152 |
inclination: | 47.2130° |
perigee height: | 1514 km |
apogee height: | 1685 km |
right ascension of ascending node: | 82.7516° |
argument of perigee: | 233.7443° |
revolutions per day: | 12.18341729 |
mean anomaly at epoch: | 125.3405° |
orbit number at epoch: | 85893 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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