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 44881U 19093C 23079.26647530 .00001912 00000-0 24558-3 0 9991
2 44881 97.8659 159.2299 0015094 13.4834 346.6770 14.82284251175621
Epoch (UTC): | 20 March 2023 06:23:43 |
Eccentricity: | 0.0015094 |
inclination: | 97.8659° |
perigee height: | 611 km |
apogee height: | 632 km |
right ascension of ascending node: | 159.2299° |
argument of perigee: | 13.4834° |
revolutions per day: | 14.82284251 |
mean anomaly at epoch: | 346.6770° |
orbit number at epoch: | 17562 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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