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 24311.59876704 -.00000040 00000-0 42707-3 0 9996
2 00051 47.2136 67.5243 0107441 248.3822 110.5491 12.18342610859533
Epoch (UTC): | 06 November 2024 14:22:13 |
Eccentricity: | 0.0107441 |
inclination: | 47.2136° |
perigee height: | 1514 km |
apogee height: | 1685 km |
right ascension of ascending node: | 67.5243° |
argument of perigee: | 248.3822° |
revolutions per day: | 12.18342610 |
mean anomaly at epoch: | 110.5491° |
orbit number at epoch: | 85953 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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