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 00029U 60002B 24313.93302898 .00003860 00000-0 56630-3 0 9994
2 00029 48.3776 283.1998 0023095 269.7369 90.0897 14.77191919455555
Epoch (UTC): | 08 November 2024 22:23:33 |
Eccentricity: | 0.0023095 |
inclination: | 48.3776° |
perigee height: | 622 km |
apogee height: | 654 km |
right ascension of ascending node: | 283.1998° |
argument of perigee: | 269.7369° |
revolutions per day: | 14.77191919 |
mean anomaly at epoch: | 90.0897° |
orbit number at epoch: | 45555 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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