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 39136U 13015G 23155.60882203 .00028258 00000-0 71590-3 0 9997
2 39136 64.8693 30.5771 0026818 273.8632 85.9439 15.39267111559743
Epoch (UTC): | 04 June 2023 14:36:42 |
Eccentricity: | 0.0026818 |
inclination: | 64.8693° |
perigee height: | 430 km |
apogee height: | 466 km |
right ascension of ascending node: | 30.5771° |
argument of perigee: | 273.8632° |
revolutions per day: | 15.39267111 |
mean anomaly at epoch: | 85.9439° |
orbit number at epoch: | 55974 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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