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 23258U 90081CP 24355.19903538 .00001080 00000-0 53341-3 0 9993
2 23258 98.6579 342.5815 0021917 173.6151 186.5309 14.19331901682435
Epoch (UTC): | 20 December 2024 04:46:36 |
Eccentricity: | 0.0021917 |
inclination: | 98.6579° |
perigee height: | 812 km |
apogee height: | 843 km |
right ascension of ascending node: | 342.5815° |
argument of perigee: | 173.6151° |
revolutions per day: | 14.19331901 |
mean anomaly at epoch: | 186.5309° |
orbit number at epoch: | 68243 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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