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 45511U 79095CT 23319.99420427 .00002111 00000-0 11128-2 0 9991
2 45511 81.2158 63.7390 0008669 330.0254 30.0421 14.13623737305833
Epoch (UTC): | 15 November 2023 23:51:39 |
Eccentricity: | 0.0008669 |
inclination: | 81.2158° |
perigee height: | 841 km |
apogee height: | 853 km |
right ascension of ascending node: | 63.7390° |
argument of perigee: | 330.0254° |
revolutions per day: | 14.13623737 |
mean anomaly at epoch: | 30.0421° |
orbit number at epoch: | 30583 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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