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 24309.55447591 .00000639 00000-0 54451-3 0 9999
2 00116 66.8092 253.4366 0079185 322.3787 37.1768 13.92138099214624
Epoch (UTC): | 04 November 2024 13:18:26 |
Eccentricity: | 0.0079185 |
inclination: | 66.8092° |
perigee height: | 863 km |
apogee height: | 979 km |
right ascension of ascending node: | 253.4366° |
argument of perigee: | 322.3787° |
revolutions per day: | 13.92138099 |
mean anomaly at epoch: | 37.1768° |
orbit number at epoch: | 21462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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