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 22178.59286477 .00005109 00000-0 24188-3 0 9993
2 40911 97.4897 182.5108 0011926 328.3664 148.5881 15.19730591374399
Epoch (UTC): | 27 June 2022 14:13:43 |
Eccentricity: | 0.0011926 |
inclination: | 97.4897° |
perigee height: | 498 km |
apogee height: | 515 km |
right ascension of ascending node: | 182.5108° |
argument of perigee: | 328.3664° |
revolutions per day: | 15.19730591 |
mean anomaly at epoch: | 148.5881° |
orbit number at epoch: | 37439 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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