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 40911U 15049N 22175.82033346 .00005916 00000-0 27972-3 0 9991
2 40911 97.4901 179.7599 0012296 338.8121 99.3580 15.19705666373979
Epoch (UTC): | 24 June 2022 19:41:16 |
Eccentricity: | 0.0012296 |
inclination: | 97.4901° |
perigee height: | 498 km |
apogee height: | 515 km |
right ascension of ascending node: | 179.7599° |
argument of perigee: | 338.8121° |
revolutions per day: | 15.19705666 |
mean anomaly at epoch: | 99.3580° |
orbit number at epoch: | 37397 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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