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 40071U 14037C 22177.85742041 .00000642 00000-0 88530-4 0 9997
2 40071 98.4084 47.0635 0007208 291.6341 68.4099 14.81882824430734
Epoch (UTC): | 26 June 2022 20:34:41 |
Eccentricity: | 0.0007208 |
inclination: | 98.4084° |
perigee height: | 618 km |
apogee height: | 628 km |
right ascension of ascending node: | 47.0635° |
argument of perigee: | 291.6341° |
revolutions per day: | 14.81882824 |
mean anomaly at epoch: | 68.4099° |
orbit number at epoch: | 43073 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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