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 43162U 18009A 23088.52954418 -.00000300 00000-0 00000-0 0 9997
2 43162 3.0234 323.1781 0002093 33.7296 159.3691 1.00272027 19059
Epoch (UTC): | 29 March 2023 12:42:32 |
Eccentricity: | 0.0002093 |
inclination: | 3.0234° |
perigee height: | 35777 km |
apogee height: | 35795 km |
right ascension of ascending node: | 323.1781° |
argument of perigee: | 33.7296° |
revolutions per day: | 1.00272027 |
mean anomaly at epoch: | 159.3691° |
orbit number at epoch: | 1905 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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