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 45502U 80073W 24262.87870142 .00009466 00000-0 37521-2 0 9992
2 45502 81.2217 317.7023 0031625 46.1369 314.2416 14.28498969509463
Epoch (UTC): | 18 September 2024 21:05:19 |
Eccentricity: | 0.0031625 |
inclination: | 81.2217° |
perigee height: | 774 km |
apogee height: | 819 km |
right ascension of ascending node: | 317.7023° |
argument of perigee: | 46.1369° |
revolutions per day: | 14.28498969 |
mean anomaly at epoch: | 314.2416° |
orbit number at epoch: | 50946 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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