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 25544U 98067A 22182.05768182 .00007735 00000-0 14443-3 0 9993
2 25544 51.6442 267.8911 0004512 318.4476 101.3651 15.49784434347339
Epoch (UTC): | 01 July 2022 01:23:03 |
Eccentricity: | 0.0004512 |
inclination: | 51.6442° |
perigee height: | 414 km |
apogee height: | 420 km |
right ascension of ascending node: | 267.8911° |
argument of perigee: | 318.4476° |
revolutions per day: | 15.49784434 |
mean anomaly at epoch: | 101.3651° |
orbit number at epoch: | 34733 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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