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 40186U 11077K 23159.91028444 -.00000085 00000-0 00000-0 0 9991
2 40186 26.6114 2.8903 7309501 146.3787 358.1697 1.88683800 78268
Epoch (UTC): | 08 June 2023 21:50:48 |
Eccentricity: | 0.7309501 |
inclination: | 26.6114° |
perigee height: | 1065 km |
apogee height: | 41506 km |
right ascension of ascending node: | 2.8903° |
argument of perigee: | 146.3787° |
revolutions per day: | 1.88683800 |
mean anomaly at epoch: | 358.1697° |
orbit number at epoch: | 7826 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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