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 44874U 19092B 23084.75019577 .00000962 00000-0 22323-3 0 9998
2 44874 98.2389 273.6769 0010833 177.3611 182.7647 14.57188802173751
Epoch (UTC): | 25 March 2023 18:00:16 |
Eccentricity: | 0.0010833 |
inclination: | 98.2389° |
perigee height: | 694 km |
apogee height: | 710 km |
right ascension of ascending node: | 273.6769° |
argument of perigee: | 177.3611° |
revolutions per day: | 14.57188802 |
mean anomaly at epoch: | 182.7647° |
orbit number at epoch: | 17375 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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