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 42759U 17034B 23084.43690326 .00019059 00000-0 98997-3 0 9991
2 42759 43.0179 220.7159 0011931 280.7084 182.6833 15.15722365318924
Epoch (UTC): | 25 March 2023 10:29:08 |
Eccentricity: | 0.0011931 |
inclination: | 43.0179° |
perigee height: | 510 km |
apogee height: | 527 km |
right ascension of ascending node: | 220.7159° |
argument of perigee: | 280.7084° |
revolutions per day: | 15.15722365 |
mean anomaly at epoch: | 182.6833° |
orbit number at epoch: | 31892 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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