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 24337.49029028 .00047965 00000-0 11445-2 0 9996
2 42761 43.0190 346.1609 0013564 64.6514 295.5746 15.40710271413254
Epoch (UTC): | 02 December 2024 11:46:01 |
Eccentricity: | 0.0013564 |
inclination: | 43.0190° |
perigee height: | 435 km |
apogee height: | 453 km |
right ascension of ascending node: | 346.1609° |
argument of perigee: | 64.6514° |
revolutions per day: | 15.40710271 |
mean anomaly at epoch: | 295.5746° |
orbit number at epoch: | 41325 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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