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 22177.13082361 .00008343 00000-0 35548-3 0 9992
2 40910 97.4719 184.1421 0011227 312.0673 114.3450 15.23160118374504
Epoch (UTC): | 26 June 2022 03:08:23 |
Eccentricity: | 0.0011227 |
inclination: | 97.4719° |
perigee height: | 488 km |
apogee height: | 504 km |
right ascension of ascending node: | 184.1421° |
argument of perigee: | 312.0673° |
revolutions per day: | 15.23160118 |
mean anomaly at epoch: | 114.3450° |
orbit number at epoch: | 37450 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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