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 40057U 14034E 23087.22673836 .00007614 00000-0 98455-3 0 9997
2 40057 98.3735 276.6327 0010833 139.0127 221.1883 14.81170900471440
Epoch (UTC): | 28 March 2023 05:26:30 |
Eccentricity: | 0.0010833 |
inclination: | 98.3735° |
perigee height: | 618 km |
apogee height: | 633 km |
right ascension of ascending node: | 276.6327° |
argument of perigee: | 139.0127° |
revolutions per day: | 14.81170900 |
mean anomaly at epoch: | 221.1883° |
orbit number at epoch: | 47144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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