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 41634U 16043A 22142.17544913 .00001529 00000-0 17729-3 0 9993
2 41634 75.0035 196.6553 0006981 34.3293 325.8333 14.86142611319759
Epoch (UTC): | 22 May 2022 04:12:38 |
Eccentricity: | 0.0006981 |
inclination: | 75.0035° |
perigee height: | 605 km |
apogee height: | 615 km |
right ascension of ascending node: | 196.6553° |
argument of perigee: | 34.3293° |
revolutions per day: | 14.86142611 |
mean anomaly at epoch: | 325.8333° |
orbit number at epoch: | 31975 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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