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 22803U 93059B 23151.25006029 -.00000122 00000-0 -36953-4 0 9994
2 22803 70.9905 347.7713 0018894 309.6697 50.2759 14.16934121536227
Epoch (UTC): | 31 May 2023 06:00:05 |
Eccentricity: | 0.0018894 |
inclination: | 70.9905° |
perigee height: | 822 km |
apogee height: | 849 km |
right ascension of ascending node: | 347.7713° |
argument of perigee: | 309.6697° |
revolutions per day: | 14.16934121 |
mean anomaly at epoch: | 50.2759° |
orbit number at epoch: | 53622 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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