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 39161U 13021C 23090.63763935 .00003455 00000-0 53310-3 0 9995
2 39161 97.8759 165.1043 0008899 211.7722 148.2933 14.73963304531754
Epoch (UTC): | 31 March 2023 15:18:12 |
Eccentricity: | 0.0008899 |
inclination: | 97.8759° |
perigee height: | 642 km |
apogee height: | 655 km |
right ascension of ascending node: | 165.1043° |
argument of perigee: | 211.7722° |
revolutions per day: | 14.73963304 |
mean anomaly at epoch: | 148.2933° |
orbit number at epoch: | 53175 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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