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 25396U 98043C 22222.14659086 .00000064 00000-0 46705-4 0 9994
2 25396 98.7976 172.1356 0001491 270.4329 89.6679 14.24677670251838
Epoch (UTC): | 10 August 2022 03:31:05 |
Eccentricity: | 0.0001491 |
inclination: | 98.7976° |
perigee height: | 808 km |
apogee height: | 810 km |
right ascension of ascending node: | 172.1356° |
argument of perigee: | 270.4329° |
revolutions per day: | 14.24677670 |
mean anomaly at epoch: | 89.6679° |
orbit number at epoch: | 25183 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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