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 40376U 15003A 23147.77182165 .00000508 00000-0 10729-3 0 9998
2 40376 98.1275 154.6311 0001304 87.5948 272.5404 14.63374665444342
Epoch (UTC): | 27 May 2023 18:31:25 |
Eccentricity: | 0.0001304 |
inclination: | 98.1275° |
perigee height: | 681 km |
apogee height: | 683 km |
right ascension of ascending node: | 154.6311° |
argument of perigee: | 87.5948° |
revolutions per day: | 14.63374665 |
mean anomaly at epoch: | 272.5404° |
orbit number at epoch: | 44434 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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