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 36203U 99025DUC 24353.97529286 .00009462 00000-0 14932-2 0 9996
2 36203 99.0867 248.5942 0096616 184.6582 175.3732 14.69521386581446
Epoch (UTC): | 18 December 2024 23:24:25 |
Eccentricity: | 0.0096616 |
inclination: | 99.0867° |
perigee height: | 594 km |
apogee height: | 730 km |
right ascension of ascending node: | 248.5942° |
argument of perigee: | 184.6582° |
revolutions per day: | 14.69521386 |
mean anomaly at epoch: | 175.3732° |
orbit number at epoch: | 58144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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