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 11U 59001A 24313.87266586 .00001788 00000-0 93044-3 0 9995
2 11 32.8694 138.2126 1454085 329.1673 23.0854 11.88896468807474
Epoch (UTC): | 08 November 2024 20:56:38 |
Eccentricity: | 0.1454085 |
inclination: | 32.8694° |
perigee height: | 552 km |
apogee height: | 2910 km |
right ascension of ascending node: | 138.2126° |
argument of perigee: | 329.1673° |
revolutions per day: | 11.88896468 |
mean anomaly at epoch: | 23.0854° |
orbit number at epoch: | 80747 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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