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 18116.91715356 +.00000230 +00000-0 +13877-3 0 9999
2 22803 070.9897 308.3305 0019438 267.8983 091.9915 14.16790849272461
Epoch (UTC): | 26 April 2018 22:00:42 |
Eccentricity: | 0.0019438 |
inclination: | 70.9897° |
perigee height: | 822 km |
apogee height: | 850 km |
right ascension of ascending node: | 308.3305° |
argument of perigee: | 267.8983° |
revolutions per day: | 14.16790849 |
mean anomaly at epoch: | 91.9915° |
orbit number at epoch: | 27246 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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