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 40911U 15049N 23080.30874322 .00018594 00000-0 74047-3 0 9998
2 40911 97.4937 88.1018 0013737 104.6021 20.8142 15.25202495414952
Epoch (UTC): | 21 March 2023 07:24:35 |
Eccentricity: | 0.0013737 |
inclination: | 97.4937° |
perigee height: | 481 km |
apogee height: | 499 km |
right ascension of ascending node: | 88.1018° |
argument of perigee: | 104.6021° |
revolutions per day: | 15.25202495 |
mean anomaly at epoch: | 20.8142° |
orbit number at epoch: | 41495 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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