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 10515U 77117B 24315.87842476 .00000223 00000-0 12096-3 0 9994
2 10515 81.2438 172.2066 0027920 160.4954 199.7291 14.08975902410214
Epoch (UTC): | 10 November 2024 21:04:55 |
Eccentricity: | 0.0027920 |
inclination: | 81.2438° |
perigee height: | 842 km |
apogee height: | 883 km |
right ascension of ascending node: | 172.2066° |
argument of perigee: | 160.4954° |
revolutions per day: | 14.08975902 |
mean anomaly at epoch: | 199.7291° |
orbit number at epoch: | 41021 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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