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 43189U 18014K 23275.65934123 .00006271 00000-0 49033-3 0 9999
2 43189 97.6131 177.2900 0014951 154.8393 205.3563 15.01334692308226
Epoch (UTC): | 02 October 2023 15:49:27 |
Eccentricity: | 0.0014951 |
inclination: | 97.6131° |
perigee height: | 552 km |
apogee height: | 573 km |
right ascension of ascending node: | 177.2900° |
argument of perigee: | 154.8393° |
revolutions per day: | 15.01334692 |
mean anomaly at epoch: | 205.3563° |
orbit number at epoch: | 30822 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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