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 25338U 98030A 24311.53556292 .00000867 00000-0 37563-3 0 9997
2 25338 98.5575 335.6339 0009150 268.4556 91.5576 14.26784546377484
Epoch (UTC): | 06 November 2024 12:51:12 |
Eccentricity: | 0.0009150 |
inclination: | 98.5575° |
perigee height: | 796 km |
apogee height: | 809 km |
right ascension of ascending node: | 335.6339° |
argument of perigee: | 268.4556° |
revolutions per day: | 14.26784546 |
mean anomaly at epoch: | 91.5576° |
orbit number at epoch: | 37748 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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