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 23149.97933317 -.00000169 00000-0 -60301-4 0 9994
2 22803 70.9907 350.4500 0018854 311.4439 48.5064 14.16934330535786
Epoch (UTC): | 29 May 2023 23:30:14 |
Eccentricity: | 0.0018854 |
inclination: | 70.9907° |
perigee height: | 822 km |
apogee height: | 849 km |
right ascension of ascending node: | 350.4500° |
argument of perigee: | 311.4439° |
revolutions per day: | 14.16934330 |
mean anomaly at epoch: | 48.5064° |
orbit number at epoch: | 53578 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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