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 23344U 94074C 24280.81998694 .00004869 00000-0 98171-3 0 9996
2 23344 97.9926 302.6253 0120362 213.5693 320.9748 14.57394628583079
Epoch (UTC): | 06 October 2024 19:40:46 |
Eccentricity: | 0.0120362 |
inclination: | 97.9926° |
perigee height: | 616 km |
apogee height: | 787 km |
right ascension of ascending node: | 302.6253° |
argument of perigee: | 213.5693° |
revolutions per day: | 14.57394628 |
mean anomaly at epoch: | 320.9748° |
orbit number at epoch: | 58307 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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