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 20441U 90005F 22181.51496226 .00000027 00000-0 26691-4 0 9991
2 20441 98.8193 151.8801 0012118 139.3949 333.9227 14.32958457694653
Epoch (UTC): | 30 June 2022 12:21:32 |
Eccentricity: | 0.0012118 |
inclination: | 98.8193° |
perigee height: | 773 km |
apogee height: | 790 km |
right ascension of ascending node: | 151.8801° |
argument of perigee: | 139.3949° |
revolutions per day: | 14.32958457 |
mean anomaly at epoch: | 333.9227° |
orbit number at epoch: | 69465 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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