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 22136.51973485 .00006747 00000-0 32306-3 0 9991
2 40911 97.4908 140.7623 0015259 105.7832 50.7766 15.19178799368000
Epoch (UTC): | 16 May 2022 12:28:25 |
Eccentricity: | 0.0015259 |
inclination: | 97.4908° |
perigee height: | 498 km |
apogee height: | 519 km |
right ascension of ascending node: | 140.7623° |
argument of perigee: | 105.7832° |
revolutions per day: | 15.19178799 |
mean anomaly at epoch: | 50.7766° |
orbit number at epoch: | 36800 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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