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 40966U 15058C 24357.99343577 .00012711 00000-0 10165-2 0 9999
2 40966 64.7653 132.3599 0179275 251.4760 106.6799 14.88683975285198
Epoch (UTC): | 22 December 2024 23:50:32 |
Eccentricity: | 0.0179275 |
inclination: | 64.7653° |
perigee height: | 477 km |
apogee height: | 727 km |
right ascension of ascending node: | 132.3599° |
argument of perigee: | 251.4760° |
revolutions per day: | 14.88683975 |
mean anomaly at epoch: | 106.6799° |
orbit number at epoch: | 28519 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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