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 43017U 17073E 23086.68330161 .00011475 00000-0 81692-3 0 9997
2 43017 97.6414 334.2548 0236884 338.5676 20.5745 14.84852715289081
Epoch (UTC): | 27 March 2023 16:23:57 |
Eccentricity: | 0.0236884 |
inclination: | 97.6414° |
perigee height: | 448 km |
apogee height: | 779 km |
right ascension of ascending node: | 334.2548° |
argument of perigee: | 338.5676° |
revolutions per day: | 14.84852715 |
mean anomaly at epoch: | 20.5745° |
orbit number at epoch: | 28908 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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