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 17291U 87001B 22148.53033806 .00000044 00000-0 25866-4 0 9990
2 17291 82.4691 210.1383 0011746 26.2397 333.9356 13.84594221788383
Epoch (UTC): | 28 May 2022 12:43:41 |
Eccentricity: | 0.0011746 |
inclination: | 82.4691° |
perigee height: | 939 km |
apogee height: | 956 km |
right ascension of ascending node: | 210.1383° |
argument of perigee: | 26.2397° |
revolutions per day: | 13.84594221 |
mean anomaly at epoch: | 333.9356° |
orbit number at epoch: | 78838 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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