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 40906U 15049H 22142.11137118 .00008837 00000-0 42649-3 0 9996
2 40906 97.4930 145.7412 0015904 90.7487 341.7173 15.18798977368927
Epoch (UTC): | 22 May 2022 02:40:22 |
Eccentricity: | 0.0015904 |
inclination: | 97.4930° |
perigee height: | 498 km |
apogee height: | 520 km |
right ascension of ascending node: | 145.7412° |
argument of perigee: | 90.7487° |
revolutions per day: | 15.18798977 |
mean anomaly at epoch: | 341.7173° |
orbit number at epoch: | 36892 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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