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 24259.93518156 .00003692 00000-0 44648-3 0 9996
2 44881 97.8224 334.9634 0014804 31.0249 329.1836 14.84230387256507
Epoch (UTC): | 15 September 2024 22:26:39 |
Eccentricity: | 0.0014804 |
inclination: | 97.8224° |
perigee height: | 605 km |
apogee height: | 626 km |
right ascension of ascending node: | 334.9634° |
argument of perigee: | 31.0249° |
revolutions per day: | 14.84230387 |
mean anomaly at epoch: | 329.1836° |
orbit number at epoch: | 25650 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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