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 35933U 09051C 22178.56452626 .00000362 00000-0 91589-4 0 9991
2 35933 98.5619 36.4072 0006541 38.8788 321.2879 14.56891824677643
Epoch (UTC): | 27 June 2022 13:32:55 |
Eccentricity: | 0.0006541 |
inclination: | 98.5619° |
perigee height: | 698 km |
apogee height: | 708 km |
right ascension of ascending node: | 36.4072° |
argument of perigee: | 38.8788° |
revolutions per day: | 14.56891824 |
mean anomaly at epoch: | 321.2879° |
orbit number at epoch: | 67764 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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