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 05707U 71114B 23151.92228496 .00000262 00000-0 92701-4 0 9990
2 05707 74.0291 32.9641 0025455 288.3707 71.4679 14.39292799695374
Epoch (UTC): | 31 May 2023 22:08:05 |
Eccentricity: | 0.0025455 |
inclination: | 74.0291° |
perigee height: | 742 km |
apogee height: | 779 km |
right ascension of ascending node: | 32.9641° |
argument of perigee: | 288.3707° |
revolutions per day: | 14.39292799 |
mean anomaly at epoch: | 71.4679° |
orbit number at epoch: | 69537 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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