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 10521U 77119B 23151.83454371 .00000262 00000-0 89290-4 0 9993
2 10521 74.0264 201.4931 0020147 41.1671 319.0999 14.41173372385142
Epoch (UTC): | 31 May 2023 20:01:44 |
Eccentricity: | 0.0020147 |
inclination: | 74.0264° |
perigee height: | 740 km |
apogee height: | 769 km |
right ascension of ascending node: | 201.4931° |
argument of perigee: | 41.1671° |
revolutions per day: | 14.41173372 |
mean anomaly at epoch: | 319.0999° |
orbit number at epoch: | 38514 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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