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 35935U 09051E 22179.82512712 .00000277 00000-0 73925-4 0 9995
2 35935 98.5718 37.7549 0008813 35.7962 324.3824 14.56000587677532
Epoch (UTC): | 28 June 2022 19:48:10 |
Eccentricity: | 0.0008813 |
inclination: | 98.5718° |
perigee height: | 700 km |
apogee height: | 712 km |
right ascension of ascending node: | 37.7549° |
argument of perigee: | 35.7962° |
revolutions per day: | 14.56000587 |
mean anomaly at epoch: | 324.3824° |
orbit number at epoch: | 67753 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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