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 40960U 15057C 22179.41098658 .00000332 00000-0 58210-4 0 9997
2 40960 97.7533 226.8031 0016613 288.6062 71.3340 14.73683853361675
Epoch (UTC): | 28 June 2022 09:51:49 |
Eccentricity: | 0.0016613 |
inclination: | 97.7533° |
perigee height: | 637 km |
apogee height: | 661 km |
right ascension of ascending node: | 226.8031° |
argument of perigee: | 288.6062° |
revolutions per day: | 14.73683853 |
mean anomaly at epoch: | 71.3340° |
orbit number at epoch: | 36167 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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