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 36048U 93036AXK 25113.69107093 .00001175 00000-0 39978-3 0 9992
2 36048 74.0586 7.7036 0026281 121.3998 270.1122 14.37438591821537
Epoch (UTC): | 23 April 2025 16:35:08 |
Eccentricity: | 0.0026281 |
inclination: | 74.0586° |
perigee height: | 748 km |
apogee height: | 786 km |
right ascension of ascending node: | 7.7036° |
argument of perigee: | 121.3998° |
revolutions per day: | 14.37438591 |
mean anomaly at epoch: | 270.1122° |
orbit number at epoch: | 82153 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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