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 23268.51255174 .00015055 00000-0 70845-3 0 9996
2 42759 43.0149 277.2116 0010285 26.0041 334.1323 15.19322582346881
Epoch (UTC): | 25 September 2023 12:18:04 |
Eccentricity: | 0.0010285 |
inclination: | 43.0149° |
perigee height: | 501 km |
apogee height: | 515 km |
right ascension of ascending node: | 277.2116° |
argument of perigee: | 26.0041° |
revolutions per day: | 15.19322582 |
mean anomaly at epoch: | 334.1323° |
orbit number at epoch: | 34688 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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