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 12175U 78026Q 22226.49807969 .00000058 00000-0 75281-4 0 9995
2 12175 99.3902 85.3185 0062757 268.2699 154.4632 13.96086008111457
Epoch (UTC): | 14 August 2022 11:57:14 |
Eccentricity: | 0.0062757 |
inclination: | 99.3902° |
perigee height: | 861 km |
apogee height: | 953 km |
right ascension of ascending node: | 85.3185° |
argument of perigee: | 268.2699° |
revolutions per day: | 13.96086008 |
mean anomaly at epoch: | 154.4632° |
orbit number at epoch: | 11145 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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