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 16613U 86019A 23159.52253611 .00000933 00000-0 15596-3 0 9990
2 16613 98.7500 7.4746 0141222 112.1366 249.4894 14.66197049648834
Epoch (UTC): | 08 June 2023 12:32:27 |
Eccentricity: | 0.0141222 |
inclination: | 98.7500° |
perigee height: | 573 km |
apogee height: | 773 km |
right ascension of ascending node: | 7.4746° |
argument of perigee: | 112.1366° |
revolutions per day: | 14.66197049 |
mean anomaly at epoch: | 249.4894° |
orbit number at epoch: | 64883 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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