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 12586U 81065B 24358.09625856 .00011553 00000-0 46694-3 0 9992
2 12586 97.6835 16.2165 0015816 115.1841 245.1038 15.24796776371632
Epoch (UTC): | 23 December 2024 02:18:36 |
Eccentricity: | 0.0015816 |
inclination: | 97.6835° |
perigee height: | 480 km |
apogee height: | 502 km |
right ascension of ascending node: | 16.2165° |
argument of perigee: | 115.1841° |
revolutions per day: | 15.24796776 |
mean anomaly at epoch: | 245.1038° |
orbit number at epoch: | 37163 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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