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 21263U 91032A 22142.88155841 .00000146 00000-0 79028-4 0 9991
2 21263 98.5136 143.4223 0014682 57.2604 302.9989 14.25989908613085
Epoch (UTC): | 22 May 2022 21:09:26 |
Eccentricity: | 0.0014682 |
inclination: | 98.5136° |
perigee height: | 794 km |
apogee height: | 816 km |
right ascension of ascending node: | 143.4223° |
argument of perigee: | 57.2604° |
revolutions per day: | 14.25989908 |
mean anomaly at epoch: | 302.9989° |
orbit number at epoch: | 61308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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