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 40545U 15017B 23336.49076862 -.00000090 00000-0 00000+0 0 9990
2 40545 56.9194 6.8595 0005214 246.0909 113.9060 1.70475805 54050
Epoch (UTC): | 02 December 2023 11:46:42 |
Eccentricity: | 0.0005214 |
inclination: | 56.9194° |
perigee height: | 23206 km |
apogee height: | 23237 km |
right ascension of ascending node: | 6.8595° |
argument of perigee: | 246.0909° |
revolutions per day: | 1.70475805 |
mean anomaly at epoch: | 113.9060° |
orbit number at epoch: | 5405 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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