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 27561U 02054C 23151.46820355 .00000431 00000-0 10684-3 0 9997
2 27561 98.5260 331.5331 0044797 318.8213 40.9607 14.56564858 88575
Epoch (UTC): | 31 May 2023 11:14:12 |
Eccentricity: | 0.0044797 |
inclination: | 98.5260° |
perigee height: | 672 km |
apogee height: | 736 km |
right ascension of ascending node: | 331.5331° |
argument of perigee: | 318.8213° |
revolutions per day: | 14.56564858 |
mean anomaly at epoch: | 40.9607° |
orbit number at epoch: | 8857 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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