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 10572U 77121P 24357.58182593 .00000370 00000-0 39765-3 0 9998
2 10572 65.0343 57.3153 0175457 164.3617 196.2960 13.79207955360773
Epoch (UTC): | 22 December 2024 13:57:49 |
Eccentricity: | 0.0175457 |
inclination: | 65.0343° |
perigee height: | 838 km |
apogee height: | 1095 km |
right ascension of ascending node: | 57.3153° |
argument of perigee: | 164.3617° |
revolutions per day: | 13.79207955 |
mean anomaly at epoch: | 196.2960° |
orbit number at epoch: | 36077 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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