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 44758C 19074AX 21021.38837044 .00007579 00000-0 50787-3 0 216
2 44758 53.0574 356.1784 0001909 55.7585 61.1131 15.06385533 15
Epoch (UTC): | 21 January 2021 09:19:15 |
Eccentricity: | 0.0001909 |
inclination: | 53.0574° |
perigee height: | 546 km |
apogee height: | 548 km |
right ascension of ascending node: | 356.1784° |
argument of perigee: | 55.7585° |
revolutions per day: | 15.06385533 |
mean anomaly at epoch: | 61.1131° |
orbit number at epoch: | 1 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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