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 18583U 87097A 23088.34899865 -.00000062 00000-0 00000-0 0 9998
2 18583 13.1425 345.4551 0021934 248.3710 295.0206 0.98387607 13156
Epoch (UTC): | 29 March 2023 08:22:33 |
Eccentricity: | 0.0021934 |
inclination: | 13.1425° |
perigee height: | 36229 km |
apogee height: | 36416 km |
right ascension of ascending node: | 345.4551° |
argument of perigee: | 248.3710° |
revolutions per day: | 0.98387607 |
mean anomaly at epoch: | 295.0206° |
orbit number at epoch: | 1315 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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