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 38759U 12048B 24357.77498170 .00012239 00000-0 66396-3 0 9991
2 38759 64.6582 130.7623 0137234 327.5475 31.7258 15.07087067 34161
Epoch (UTC): | 22 December 2024 18:35:58 |
Eccentricity: | 0.0137234 |
inclination: | 64.6582° |
perigee height: | 450 km |
apogee height: | 640 km |
right ascension of ascending node: | 130.7623° |
argument of perigee: | 327.5475° |
revolutions per day: | 15.07087067 |
mean anomaly at epoch: | 31.7258° |
orbit number at epoch: | 3416 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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