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 43614U 18070B 23025.50947805 .12862050 16659-6 28667-3 0 9993
2 43614 92.9763 194.5607 0009679 275.6467 84.3741 16.45985663245894
Epoch (UTC): | 25 January 2023 12:13:38 |
Eccentricity: | 0.0009679 |
inclination: | 92.9763° |
perigee height: | 143 km |
apogee height: | 156 km |
right ascension of ascending node: | 194.5607° |
argument of perigee: | 275.6467° |
revolutions per day: | 16.45985663 |
mean anomaly at epoch: | 84.3741° |
orbit number at epoch: | 24589 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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