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 23081.34928025 .00006508 00000-0 84461-3 0 9990
2 40057 98.3733 270.4945 0010768 158.5505 201.6060 14.81080093470575
Epoch (UTC): | 22 March 2023 08:22:57 |
Eccentricity: | 0.0010768 |
inclination: | 98.3733° |
perigee height: | 618 km |
apogee height: | 633 km |
right ascension of ascending node: | 270.4945° |
argument of perigee: | 158.5505° |
revolutions per day: | 14.81080093 |
mean anomaly at epoch: | 201.6060° |
orbit number at epoch: | 47057 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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