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 24315.92183833 .00107260 00000-0 30820-2 0 9996
2 33493 98.1828 17.4716 0008437 99.3379 260.8817 15.35361723861416
Epoch (UTC): | 10 November 2024 22:07:26 |
Eccentricity: | 0.0008437 |
inclination: | 98.1828° |
perigee height: | 454 km |
apogee height: | 465 km |
right ascension of ascending node: | 17.4716° |
argument of perigee: | 99.3379° |
revolutions per day: | 15.35361723 |
mean anomaly at epoch: | 260.8817° |
orbit number at epoch: | 86141 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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