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 40910U 15049M 23079.22185365 .00035817 00000-0 11502-2 0 9991
2 40910 97.4702 91.2339 0013119 84.4744 340.7139 15.32125091415240
Epoch (UTC): | 20 March 2023 05:19:28 |
Eccentricity: | 0.0013119 |
inclination: | 97.4702° |
perigee height: | 460 km |
apogee height: | 478 km |
right ascension of ascending node: | 91.2339° |
argument of perigee: | 84.4744° |
revolutions per day: | 15.32125091 |
mean anomaly at epoch: | 340.7139° |
orbit number at epoch: | 41524 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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