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 42761U 17034D 23341.83906469 .00007657 00000-0 34263-3 0 9999
2 42761 43.0136 226.1525 0011314 163.3777 196.7446 15.21615359358052
Epoch (UTC): | 07 December 2023 20:08:15 |
Eccentricity: | 0.0011314 |
inclination: | 43.0136° |
perigee height: | 493 km |
apogee height: | 509 km |
right ascension of ascending node: | 226.1525° |
argument of perigee: | 163.3777° |
revolutions per day: | 15.21615359 |
mean anomaly at epoch: | 196.7446° |
orbit number at epoch: | 35805 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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