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 23157.55648393 .00005618 00000-0 26654-3 0 9997
2 40908 97.5243 160.6444 0012773 220.9889 139.0386 15.19606215426183
Epoch (UTC): | 06 June 2023 13:21:20 |
Eccentricity: | 0.0012773 |
inclination: | 97.5243° |
perigee height: | 498 km |
apogee height: | 516 km |
right ascension of ascending node: | 160.6444° |
argument of perigee: | 220.9889° |
revolutions per day: | 15.19606215 |
mean anomaly at epoch: | 139.0386° |
orbit number at epoch: | 42618 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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