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 00116U 61015A 24316.52311480 .00000406 00000-0 36743-3 0 9997
2 00116 66.8095 236.3906 0079573 317.8253 41.6721 13.92146815215596
Epoch (UTC): | 11 November 2024 12:33:17 |
Eccentricity: | 0.0079573 |
inclination: | 66.8095° |
perigee height: | 863 km |
apogee height: | 979 km |
right ascension of ascending node: | 236.3906° |
argument of perigee: | 317.8253° |
revolutions per day: | 13.92146815 |
mean anomaly at epoch: | 41.6721° |
orbit number at epoch: | 21559 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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