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 42828U 17042D 22222.85075799 .00001425 00000-0 14194-3 0 9992
2 42828 97.4251 76.1653 0013876 175.4972 184.6376 14.92999743276267
Epoch (UTC): | 10 August 2022 20:25:05 |
Eccentricity: | 0.0013876 |
inclination: | 97.4251° |
perigee height: | 579 km |
apogee height: | 598 km |
right ascension of ascending node: | 76.1653° |
argument of perigee: | 175.4972° |
revolutions per day: | 14.92999743 |
mean anomaly at epoch: | 184.6376° |
orbit number at epoch: | 27626 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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