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 25876U 99041E 23027.48498548 .00003052 00000-0 55211-3 0 9992
2 25876 51.7660 142.0147 0527107 248.0656 106.3459 14.05607191202722
Epoch (UTC): | 27 January 2023 11:38:22 |
Eccentricity: | 0.0527107 |
inclination: | 51.7660° |
perigee height: | 492 km |
apogee height: | 1257 km |
right ascension of ascending node: | 142.0147° |
argument of perigee: | 248.0656° |
revolutions per day: | 14.05607191 |
mean anomaly at epoch: | 106.3459° |
orbit number at epoch: | 20272 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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