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 14781U 84021B 23333.92343992 .00003546 00000-0 41471-3 0 9999
2 14781 97.6800 304.7023 0008844 27.3785 332.7895 14.85676110139748
Epoch (UTC): | 29 November 2023 22:09:45 |
Eccentricity: | 0.0008844 |
inclination: | 97.6800° |
perigee height: | 605 km |
apogee height: | 617 km |
right ascension of ascending node: | 304.7023° |
argument of perigee: | 27.3785° |
revolutions per day: | 14.85676110 |
mean anomaly at epoch: | 332.7895° |
orbit number at epoch: | 13974 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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