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 10114U 77057B 24358.22413278 .00015657 00000-0 47915-3 0 9997
2 10114 97.5301 145.0375 0010444 72.6149 287.6234 15.33872346600618
Epoch (UTC): | 23 December 2024 05:22:45 |
Eccentricity: | 0.0010444 |
inclination: | 97.5301° |
perigee height: | 457 km |
apogee height: | 471 km |
right ascension of ascending node: | 145.0375° |
argument of perigee: | 72.6149° |
revolutions per day: | 15.33872346 |
mean anomaly at epoch: | 287.6234° |
orbit number at epoch: | 60061 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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