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 40043U 14033AK 24278.16458119 .00009616 00000-0 12425-2 0 9998
2 40043 97.7080 76.3450 0053283 308.9851 50.6621 14.80135675553872
Epoch (UTC): | 04 October 2024 03:56:59 |
Eccentricity: | 0.0053283 |
inclination: | 97.7080° |
perigee height: | 591 km |
apogee height: | 666 km |
right ascension of ascending node: | 76.3450° |
argument of perigee: | 308.9851° |
revolutions per day: | 14.80135675 |
mean anomaly at epoch: | 50.6621° |
orbit number at epoch: | 55387 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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