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 59224U 24047A 24358.09133401 .00013491 00000-0 89168-3 0 9995
2 59224 97.6025 321.5731 0018445 120.7966 239.5080 15.07371799 42886
Epoch (UTC): | 23 December 2024 02:11:31 |
Eccentricity: | 0.0018445 |
inclination: | 97.6025° |
perigee height: | 531 km |
apogee height: | 557 km |
right ascension of ascending node: | 321.5731° |
argument of perigee: | 120.7966° |
revolutions per day: | 15.07371799 |
mean anomaly at epoch: | 239.5080° |
orbit number at epoch: | 4288 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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