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 41503U 00055MB 22222.06448614 .00002404 00000-0 10537-2 0 9994
2 41503 98.7651 315.5422 0034282 284.3867 75.3507 14.24302343333473
Epoch (UTC): | 10 August 2022 01:32:51 |
Eccentricity: | 0.0034282 |
inclination: | 98.7651° |
perigee height: | 786 km |
apogee height: | 835 km |
right ascension of ascending node: | 315.5422° |
argument of perigee: | 284.3867° |
revolutions per day: | 14.24302343 |
mean anomaly at epoch: | 75.3507° |
orbit number at epoch: | 33347 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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