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 27844U 03031E 22178.55558304 .00000159 00000-0 90779-4 0 9998
2 27844 98.6777 186.0891 0011117 74.9821 285.2587 14.22459263985306
Epoch (UTC): | 27 June 2022 13:20:02 |
Eccentricity: | 0.0011117 |
inclination: | 98.6777° |
perigee height: | 809 km |
apogee height: | 825 km |
right ascension of ascending node: | 186.0891° |
argument of perigee: | 74.9821° |
revolutions per day: | 14.22459263 |
mean anomaly at epoch: | 285.2587° |
orbit number at epoch: | 98530 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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