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 17911U 87038A 23266.81794952 .00007715 00000-0 36049-3 0 9994
2 17911 82.5174 108.3134 0007846 260.7843 99.2505 15.19623901988027
Epoch (UTC): | 23 September 2023 19:37:50 |
Eccentricity: | 0.0007846 |
inclination: | 82.5174° |
perigee height: | 501 km |
apogee height: | 512 km |
right ascension of ascending node: | 108.3134° |
argument of perigee: | 260.7843° |
revolutions per day: | 15.19623901 |
mean anomaly at epoch: | 99.2505° |
orbit number at epoch: | 98802 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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