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 20442U 90005G 22177.45691744 .00000054 00000-0 36306-4 0 9996
2 20442 98.7941 142.4559 0012445 138.1639 222.0498 14.33066374694394
Epoch (UTC): | 26 June 2022 10:57:57 |
Eccentricity: | 0.0012445 |
inclination: | 98.7941° |
perigee height: | 772 km |
apogee height: | 790 km |
right ascension of ascending node: | 142.4559° |
argument of perigee: | 138.1639° |
revolutions per day: | 14.33066374 |
mean anomaly at epoch: | 222.0498° |
orbit number at epoch: | 69439 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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