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 22565U 93016A 24305.87434879 .00000014 00000-0 33924-4 0 9993
2 22565 70.8110 127.2559 0004188 51.6464 308.5031 14.12523898629849
Epoch (UTC): | 31 October 2024 20:59:03 |
Eccentricity: | 0.0004188 |
inclination: | 70.8110° |
perigee height: | 848 km |
apogee height: | 854 km |
right ascension of ascending node: | 127.2559° |
argument of perigee: | 51.6464° |
revolutions per day: | 14.12523898 |
mean anomaly at epoch: | 308.5031° |
orbit number at epoch: | 62984 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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