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 37326U 93036BKS 24279.72693843 .00012277 00000-0 26261-2 0 9996
2 37326 74.0260 81.4790 0060758 318.1216 41.5308 14.57663151791646
Epoch (UTC): | 05 October 2024 17:26:47 |
Eccentricity: | 0.0060758 |
inclination: | 74.0260° |
perigee height: | 658 km |
apogee height: | 744 km |
right ascension of ascending node: | 81.4790° |
argument of perigee: | 318.1216° |
revolutions per day: | 14.57663151 |
mean anomaly at epoch: | 41.5308° |
orbit number at epoch: | 79164 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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