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 40071U 14037C 23087.89186201 .00003020 00000-0 38137-3 0 9992
2 40071 98.3709 335.2340 0009165 118.3328 241.8794 14.82683075471479
Epoch (UTC): | 28 March 2023 21:24:16 |
Eccentricity: | 0.0009165 |
inclination: | 98.3709° |
perigee height: | 614 km |
apogee height: | 627 km |
right ascension of ascending node: | 335.2340° |
argument of perigee: | 118.3328° |
revolutions per day: | 14.82683075 |
mean anomaly at epoch: | 241.8794° |
orbit number at epoch: | 47147 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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