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 40967U 15058D 24262.53673336 .00006163 00000-0 55633-3 0 9998
2 40967 64.7756 89.0177 0190633 275.7373 82.2029 14.83497292 18833
Epoch (UTC): | 18 September 2024 12:52:53 |
Eccentricity: | 0.0190633 |
inclination: | 64.7756° |
perigee height: | 485 km |
apogee height: | 751 km |
right ascension of ascending node: | 89.0177° |
argument of perigee: | 275.7373° |
revolutions per day: | 14.83497292 |
mean anomaly at epoch: | 82.2029° |
orbit number at epoch: | 1883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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