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 23090.43398263 .00003497 00000-0 53953-3 0 9990
2 39161 97.8764 164.9072 0008849 212.2502 147.8158 14.73962241531726
Epoch (UTC): | 31 March 2023 10:24:56 |
Eccentricity: | 0.0008849 |
inclination: | 97.8764° |
perigee height: | 642 km |
apogee height: | 654 km |
right ascension of ascending node: | 164.9072° |
argument of perigee: | 212.2502° |
revolutions per day: | 14.73962241 |
mean anomaly at epoch: | 147.8158° |
orbit number at epoch: | 53172 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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