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 40908U 15049K 23080.31365091 .00008336 00000-0 40664-3 0 9994
2 40908 97.5261 83.6894 0016011 131.3575 356.4113 15.18448255414459
Epoch (UTC): | 21 March 2023 07:31:39 |
Eccentricity: | 0.0016011 |
inclination: | 97.5261° |
perigee height: | 499 km |
apogee height: | 521 km |
right ascension of ascending node: | 83.6894° |
argument of perigee: | 131.3575° |
revolutions per day: | 15.18448255 |
mean anomaly at epoch: | 356.4113° |
orbit number at epoch: | 41445 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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