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 40056U 14034D 22176.89027163 .00000497 00000-0 81109-4 0 9994
2 40056 98.3567 334.0942 0013471 336.2719 23.7866 14.75442612420775
Epoch (UTC): | 25 June 2022 21:21:59 |
Eccentricity: | 0.0013471 |
inclination: | 98.3567° |
perigee height: | 634 km |
apogee height: | 653 km |
right ascension of ascending node: | 334.0942° |
argument of perigee: | 336.2719° |
revolutions per day: | 14.75442612 |
mean anomaly at epoch: | 23.7866° |
orbit number at epoch: | 42077 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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