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 36519U 10017A 23332.21572441 .00000108 00000-0 10256-3 0 9998
2 36519 82.9623 214.4046 0035684 194.1089 284.0482 13.71531266680170
Epoch (UTC): | 28 November 2023 05:10:38 |
Eccentricity: | 0.0035684 |
inclination: | 82.9623° |
perigee height: | 968 km |
apogee height: | 1020 km |
right ascension of ascending node: | 214.4046° |
argument of perigee: | 194.1089° |
revolutions per day: | 13.71531266 |
mean anomaly at epoch: | 284.0482° |
orbit number at epoch: | 68017 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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