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 23089.75922581 .00052851 00000-0 15623-2 0 9993
2 39136 64.8695 249.4210 0026077 280.2368 79.5825 15.34284011549626
Epoch (UTC): | 30 March 2023 18:13:17 |
Eccentricity: | 0.0026077 |
inclination: | 64.8695° |
perigee height: | 445 km |
apogee height: | 481 km |
right ascension of ascending node: | 249.4210° |
argument of perigee: | 280.2368° |
revolutions per day: | 15.34284011 |
mean anomaly at epoch: | 79.5825° |
orbit number at epoch: | 54962 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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