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 40900U 15049B 22177.17704969 .00022789 00000-0 64339-3 0 9990
2 40900 97.4001 195.2006 0006575 243.9432 180.7916 15.36362184375959
Epoch (UTC): | 26 June 2022 04:14:57 |
Eccentricity: | 0.0006575 |
inclination: | 97.4001° |
perigee height: | 452 km |
apogee height: | 461 km |
right ascension of ascending node: | 195.2006° |
argument of perigee: | 243.9432° |
revolutions per day: | 15.36362184 |
mean anomaly at epoch: | 180.7916° |
orbit number at epoch: | 37595 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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