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 14914U 78026GP 23333.03310248 .00002468 00000-0 81399-3 0 9990
2 14914 98.6308 347.3856 0045412 173.1380 243.5672 14.38398474184171
Epoch (UTC): | 29 November 2023 00:47:40 |
Eccentricity: | 0.0045412 |
inclination: | 98.6308° |
perigee height: | 731 km |
apogee height: | 796 km |
right ascension of ascending node: | 347.3856° |
argument of perigee: | 173.1380° |
revolutions per day: | 14.38398474 |
mean anomaly at epoch: | 243.5672° |
orbit number at epoch: | 18417 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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