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 24316.55179005 .00007595 00000-0 67580-3 0 9996
2 60235 61.9952 91.5612 0027343 344.6119 15.4134 14.96552124 18658
Epoch (UTC): | 11 November 2024 13:14:34 |
Eccentricity: | 0.0027343 |
inclination: | 61.9952° |
perigee height: | 558 km |
apogee height: | 596 km |
right ascension of ascending node: | 91.5612° |
argument of perigee: | 344.6119° |
revolutions per day: | 14.96552124 |
mean anomaly at epoch: | 15.4134° |
orbit number at epoch: | 1865 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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