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 39430U 13066Q 23086.10627842 .00003116 00000-0 55120-3 0 9991
2 39430 97.7868 342.0140 0144882 232.7266 126.0652 14.61408698497554
Epoch (UTC): | 27 March 2023 02:33:02 |
Eccentricity: | 0.0144882 |
inclination: | 97.7868° |
perigee height: | 586 km |
apogee height: | 791 km |
right ascension of ascending node: | 342.0140° |
argument of perigee: | 232.7266° |
revolutions per day: | 14.61408698 |
mean anomaly at epoch: | 126.0652° |
orbit number at epoch: | 49755 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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