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 22176.91210673 .00000686 00000-0 94089-4 0 9998
2 40071 98.4083 46.0713 0007231 294.8225 65.2225 14.81881969430590
Epoch (UTC): | 25 June 2022 21:53:26 |
Eccentricity: | 0.0007231 |
inclination: | 98.4083° |
perigee height: | 618 km |
apogee height: | 628 km |
right ascension of ascending node: | 46.0713° |
argument of perigee: | 294.8225° |
revolutions per day: | 14.81881969 |
mean anomaly at epoch: | 65.2225° |
orbit number at epoch: | 43059 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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