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 00264U 61015CL 24310.54388029 .00009252 00000-0 32892-2 0 9998
2 00264 66.5278 1.4514 0015847 77.1674 283.1194 14.34629592249064
Epoch (UTC): | 05 November 2024 13:03:11 |
Eccentricity: | 0.0015847 |
inclination: | 66.5278° |
perigee height: | 765 km |
apogee height: | 787 km |
right ascension of ascending node: | 1.4514° |
argument of perigee: | 77.1674° |
revolutions per day: | 14.34629592 |
mean anomaly at epoch: | 283.1194° |
orbit number at epoch: | 24906 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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