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 22177.47553633 .00008240 00000-0 35107-3 0 9991
2 40910 97.4720 184.4851 0011235 310.6518 204.7405 15.23165137374552
Epoch (UTC): | 26 June 2022 11:24:46 |
Eccentricity: | 0.0011235 |
inclination: | 97.4720° |
perigee height: | 488 km |
apogee height: | 504 km |
right ascension of ascending node: | 184.4851° |
argument of perigee: | 310.6518° |
revolutions per day: | 15.23165137 |
mean anomaly at epoch: | 204.7405° |
orbit number at epoch: | 37455 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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