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 38135U 99025EQG 22225.94800032 .00000409 00000-0 16371-3 0 9998
2 38135 98.8209 276.1715 0237270 350.8184 8.8691 14.19793750437447
Epoch (UTC): | 13 August 2022 22:45:07 |
Eccentricity: | 0.0237270 |
inclination: | 98.8209° |
perigee height: | 655 km |
apogee height: | 997 km |
right ascension of ascending node: | 276.1715° |
argument of perigee: | 350.8184° |
revolutions per day: | 14.19793750 |
mean anomaly at epoch: | 8.8691° |
orbit number at epoch: | 43744 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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