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 116U 61015A 24313.21840472 .00000573 00000-0 49437-3 0 9997
2 116 66.8094 244.4741 0079411 319.9604 39.5637 13.92143374215630
Epoch (UTC): | 08 November 2024 05:14:30 |
Eccentricity: | 0.0079411 |
inclination: | 66.8094° |
perigee height: | 863 km |
apogee height: | 979 km |
right ascension of ascending node: | 244.4741° |
argument of perigee: | 319.9604° |
revolutions per day: | 13.92143374 |
mean anomaly at epoch: | 39.5637° |
orbit number at epoch: | 21563 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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