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 30880U 99025AXS 22228.84326584 .00001103 00000-0 58643-3 0 9994
2 30880 98.8936 286.0539 0024364 350.9939 9.0794 14.15446801795277
Epoch (UTC): | 16 August 2022 20:14:18 |
Eccentricity: | 0.0024364 |
inclination: | 98.8936° |
perigee height: | 823 km |
apogee height: | 858 km |
right ascension of ascending node: | 286.0539° |
argument of perigee: | 350.9939° |
revolutions per day: | 14.15446801 |
mean anomaly at epoch: | 9.0794° |
orbit number at epoch: | 79527 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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