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 14808U 80056C 24358.01253413 .00002864 00000-0 77746-3 0 9995
2 14808 74.0366 200.6183 0014075 291.5902 219.0501 14.47993075150872
Epoch (UTC): | 23 December 2024 00:18:02 |
Eccentricity: | 0.0014075 |
inclination: | 74.0366° |
perigee height: | 722 km |
apogee height: | 742 km |
right ascension of ascending node: | 200.6183° |
argument of perigee: | 291.5902° |
revolutions per day: | 14.47993075 |
mean anomaly at epoch: | 219.0501° |
orbit number at epoch: | 15087 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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