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 23090.09931106 .00001863 00000-0 42114-3 0 9994
2 35933 98.5263 319.9724 0004501 258.3232 101.7461 14.57449687717996
Epoch (UTC): | 31 March 2023 02:23:00 |
Eccentricity: | 0.0004501 |
inclination: | 98.5263° |
perigee height: | 698 km |
apogee height: | 704 km |
right ascension of ascending node: | 319.9724° |
argument of perigee: | 258.3232° |
revolutions per day: | 14.57449687 |
mean anomaly at epoch: | 101.7461° |
orbit number at epoch: | 71799 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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