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 43255U 18030G 23340.33685612 -.00000260 00000-0 -10000-3 0 9991
2 43255 86.3943 316.5654 0002032 83.6754 276.4673 14.34218151297759
Epoch (UTC): | 06 December 2023 08:05:04 |
Eccentricity: | 0.0002032 |
inclination: | 86.3943° |
perigee height: | 776 km |
apogee height: | 779 km |
right ascension of ascending node: | 316.5654° |
argument of perigee: | 83.6754° |
revolutions per day: | 14.34218151 |
mean anomaly at epoch: | 276.4673° |
orbit number at epoch: | 29775 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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