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 44909U 19096E 22177.57250492 .00000034 00000-0 99928-4 0 9992
2 44909 82.5209 224.2173 0216300 298.5769 59.3717 12.79713607116679
Epoch (UTC): | 26 June 2022 13:44:24 |
Eccentricity: | 0.0216300 |
inclination: | 82.5209° |
perigee height: | 1175 km |
apogee height: | 1509 km |
right ascension of ascending node: | 224.2173° |
argument of perigee: | 298.5769° |
revolutions per day: | 12.79713607 |
mean anomaly at epoch: | 59.3717° |
orbit number at epoch: | 11667 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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