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 36350U 82025AL 23337.45702876 .00004897 00000-0 22553-2 0 9998
2 36350 82.5187 237.3755 0013393 259.4818 100.4854 14.20885837539890
Epoch (UTC): | 03 December 2023 10:58:07 |
Eccentricity: | 0.0013393 |
inclination: | 82.5187° |
perigee height: | 813 km |
apogee height: | 832 km |
right ascension of ascending node: | 237.3755° |
argument of perigee: | 259.4818° |
revolutions per day: | 14.20885837 |
mean anomaly at epoch: | 100.4854° |
orbit number at epoch: | 53989 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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