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 43693U 18088D 23031.76832194 .15730055 -15917-5 67726-3 0 9995
2 43693 84.9840 152.3214 0011771 313.8197 46.2135 16.42399369235651
Epoch (UTC): | 31 January 2023 18:26:23 |
Eccentricity: | 0.0011771 |
inclination: | 84.9840° |
perigee height: | 152 km |
apogee height: | 167 km |
right ascension of ascending node: | 152.3214° |
argument of perigee: | 313.8197° |
revolutions per day: | 16.42399369 |
mean anomaly at epoch: | 46.2135° |
orbit number at epoch: | 23565 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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