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 43729U 18096L 23054.18567061 .13428813 24562-5 11607-2 0 9998
2 43729 97.2831 147.4561 0012266 283.3519 76.6412 16.39205242237005
Epoch (UTC): | 23 February 2023 04:27:21 |
Eccentricity: | 0.0012266 |
inclination: | 97.2831° |
perigee height: | 160 km |
apogee height: | 176 km |
right ascension of ascending node: | 147.4561° |
argument of perigee: | 283.3519° |
revolutions per day: | 16.39205242 |
mean anomaly at epoch: | 76.6412° |
orbit number at epoch: | 23700 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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