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 22144.91639052 .00000152 00000-0 81261-4 0 9997
2 21263 98.5135 145.4001 0014607 51.7324 308.5169 14.25990635613378
Epoch (UTC): | 24 May 2022 21:59:36 |
Eccentricity: | 0.0014607 |
inclination: | 98.5135° |
perigee height: | 794 km |
apogee height: | 815 km |
right ascension of ascending node: | 145.4001° |
argument of perigee: | 51.7324° |
revolutions per day: | 14.25990635 |
mean anomaly at epoch: | 308.5169° |
orbit number at epoch: | 61337 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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