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 23080.26832692 .00006911 00000-0 89655-3 0 9992
2 40057 98.3733 269.3651 0010757 162.4004 197.7478 14.81069247470411
Epoch (UTC): | 21 March 2023 06:26:23 |
Eccentricity: | 0.0010757 |
inclination: | 98.3733° |
perigee height: | 618 km |
apogee height: | 633 km |
right ascension of ascending node: | 269.3651° |
argument of perigee: | 162.4004° |
revolutions per day: | 14.81069247 |
mean anomaly at epoch: | 197.7478° |
orbit number at epoch: | 47041 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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