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 23083.56266206 .00002104 00000-0 48396-3 0 9999
2 35935 98.5371 313.2544 0006912 287.5893 72.4548 14.56493324716647
Epoch (UTC): | 24 March 2023 13:30:14 |
Eccentricity: | 0.0006912 |
inclination: | 98.5371° |
perigee height: | 699 km |
apogee height: | 709 km |
right ascension of ascending node: | 313.2544° |
argument of perigee: | 287.5893° |
revolutions per day: | 14.56493324 |
mean anomaly at epoch: | 72.4548° |
orbit number at epoch: | 71664 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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