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 24257.55638966 .00053521 00000-0 16325-2 0 9995
2 42759 43.0153 85.5904 0013108 230.5970 129.3723 15.33079730400947
Epoch (UTC): | 13 September 2024 13:21:12 |
Eccentricity: | 0.0013108 |
inclination: | 43.0153° |
perigee height: | 457 km |
apogee height: | 475 km |
right ascension of ascending node: | 85.5904° |
argument of perigee: | 230.5970° |
revolutions per day: | 15.33079730 |
mean anomaly at epoch: | 129.3723° |
orbit number at epoch: | 40094 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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