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 11111U 78105A 24358.12325330 .00000344 00000-0 13003-3 0 9998
2 11111 74.0261 247.4868 0015579 135.2352 225.0060 14.34966958410784
Epoch (UTC): | 23 December 2024 02:57:29 |
Eccentricity: | 0.0015579 |
inclination: | 74.0261° |
perigee height: | 764 km |
apogee height: | 786 km |
right ascension of ascending node: | 247.4868° |
argument of perigee: | 135.2352° |
revolutions per day: | 14.34966958 |
mean anomaly at epoch: | 225.0060° |
orbit number at epoch: | 41078 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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