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 60235U 24128A 24315.88363108 .00009224 00000-0 81704-3 0 9995
2 60235 61.9951 93.8688 0027225 344.2900 15.7341 14.96542737 18559
Epoch (UTC): | 10 November 2024 21:12:25 |
Eccentricity: | 0.0027225 |
inclination: | 61.9951° |
perigee height: | 558 km |
apogee height: | 596 km |
right ascension of ascending node: | 93.8688° |
argument of perigee: | 344.2900° |
revolutions per day: | 14.96542737 |
mean anomaly at epoch: | 15.7341° |
orbit number at epoch: | 1855 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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