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 33493U 09002B 23341.83094858 .00010377 00000-0 61941-3 0 9993
2 33493 98.2336 9.0121 0014264 177.2806 182.8502 15.11257324809932
Epoch (UTC): | 07 December 2023 19:56:33 |
Eccentricity: | 0.0014264 |
inclination: | 98.2336° |
perigee height: | 522 km |
apogee height: | 542 km |
right ascension of ascending node: | 9.0121° |
argument of perigee: | 177.2806° |
revolutions per day: | 15.11257324 |
mean anomaly at epoch: | 182.8502° |
orbit number at epoch: | 80993 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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