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 23328.41074497 -.00000036 00000-0 00000-0 0 9999
2 40186 26.2457 321.5420 7314571 216.1121 354.3977 1.88729758 81446
Epoch (UTC): | 24 November 2023 09:51:28 |
Eccentricity: | 0.7314571 |
inclination: | 26.2457° |
perigee height: | 1049 km |
apogee height: | 41512 km |
right ascension of ascending node: | 321.5420° |
argument of perigee: | 216.1121° |
revolutions per day: | 1.88729758 |
mean anomaly at epoch: | 354.3977° |
orbit number at epoch: | 8144 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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