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 18187U 87060A 23150.71812442 -.00000042 00000-0 21835-4 0 9996
2 18187 65.0109 265.6531 0014227 277.3580 82.5887 14.31208175874801
Epoch (UTC): | 30 May 2023 17:14:05 |
Eccentricity: | 0.0014227 |
inclination: | 65.0109° |
perigee height: | 777 km |
apogee height: | 798 km |
right ascension of ascending node: | 265.6531° |
argument of perigee: | 277.3580° |
revolutions per day: | 14.31208175 |
mean anomaly at epoch: | 82.5887° |
orbit number at epoch: | 87480 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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