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 23405U 94077B 22147.90625227 .00000043 00000-0 46815-4 0 9995
2 23405 70.9835 18.7049 0000830 148.0085 212.1088 14.15255526420716
Epoch (UTC): | 27 May 2022 21:45:00 |
Eccentricity: | 0.0000830 |
inclination: | 70.9835° |
perigee height: | 841 km |
apogee height: | 842 km |
right ascension of ascending node: | 18.7049° |
argument of perigee: | 148.0085° |
revolutions per day: | 14.15255526 |
mean anomaly at epoch: | 212.1088° |
orbit number at epoch: | 42071 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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