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 05175U 71035B 23151.77269284 .00000244 00000-0 88140-4 0 9996
2 05175 74.0464 167.0586 0030224 199.3573 160.6436 14.38359252727257
Epoch (UTC): | 31 May 2023 18:32:40 |
Eccentricity: | 0.0030224 |
inclination: | 74.0464° |
perigee height: | 742 km |
apogee height: | 785 km |
right ascension of ascending node: | 167.0586° |
argument of perigee: | 199.3573° |
revolutions per day: | 14.38359252 |
mean anomaly at epoch: | 160.6436° |
orbit number at epoch: | 72725 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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