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 5175U 71035B 23161.23172978 .00000280 00000-0 10008-3 0 9998
2 5175 74.0463 149.6398 0029828 179.7241 180.3935 14.38364885728886
Epoch (UTC): | 10 June 2023 05:33:41 |
Eccentricity: | 0.0029828 |
inclination: | 74.0463° |
perigee height: | 742 km |
apogee height: | 785 km |
right ascension of ascending node: | 149.6398° |
argument of perigee: | 179.7241° |
revolutions per day: | 14.38364885 |
mean anomaly at epoch: | 180.3935° |
orbit number at epoch: | 72888 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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