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 23159.59777194 .00005296 00000-0 25130-3 0 9995
2 40908 97.5247 162.6796 0012952 213.3258 146.7162 15.19629932426496
Epoch (UTC): | 08 June 2023 14:20:47 |
Eccentricity: | 0.0012952 |
inclination: | 97.5247° |
perigee height: | 498 km |
apogee height: | 516 km |
right ascension of ascending node: | 162.6796° |
argument of perigee: | 213.3258° |
revolutions per day: | 15.19629932 |
mean anomaly at epoch: | 146.7162° |
orbit number at epoch: | 42649 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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