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 40012U 14033C 23341.44883724 .00002683 00000-0 36954-3 0 9990
2 40012 97.6821 147.2557 0053750 212.1393 147.6538 14.78050343509355
Epoch (UTC): | 07 December 2023 10:46:19 |
Eccentricity: | 0.0053750 |
inclination: | 97.6821° |
perigee height: | 598 km |
apogee height: | 673 km |
right ascension of ascending node: | 147.2557° |
argument of perigee: | 212.1393° |
revolutions per day: | 14.78050343 |
mean anomaly at epoch: | 147.6538° |
orbit number at epoch: | 50935 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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