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 31132U 07012Q 24308.88273128 .00008922 00000-0 16492-2 0 9991
2 31132 98.3650 269.4781 0075401 11.9794 348.3179 14.63795456933895
Epoch (UTC): | 03 November 2024 21:11:07 |
Eccentricity: | 0.0075401 |
inclination: | 98.3650° |
perigee height: | 628 km |
apogee height: | 734 km |
right ascension of ascending node: | 269.4781° |
argument of perigee: | 11.9794° |
revolutions per day: | 14.63795456 |
mean anomaly at epoch: | 348.3179° |
orbit number at epoch: | 93389 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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