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 18009U 87043E 23081.09978697 .00016705 00000-0 10836-2 0 9998
2 18009 63.2996 354.4472 0930171 82.2881 288.2629 13.54192878183247
Epoch (UTC): | 22 March 2023 02:23:41 |
Eccentricity: | 0.0930171 |
inclination: | 63.2996° |
perigee height: | 365 km |
apogee height: | 1748 km |
right ascension of ascending node: | 354.4472° |
argument of perigee: | 82.2881° |
revolutions per day: | 13.54192878 |
mean anomaly at epoch: | 288.2629° |
orbit number at epoch: | 18324 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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