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 22180.55622919 .00000285 00000-0 74327-4 0 9992
2 35933 98.5615 38.4529 0006440 33.7183 326.4423 14.56893157677934
Epoch (UTC): | 29 June 2022 13:20:58 |
Eccentricity: | 0.0006440 |
inclination: | 98.5615° |
perigee height: | 698 km |
apogee height: | 708 km |
right ascension of ascending node: | 38.4529° |
argument of perigee: | 33.7183° |
revolutions per day: | 14.56893157 |
mean anomaly at epoch: | 326.4423° |
orbit number at epoch: | 67793 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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