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 12586U 81065B 22142.91566538 .00004217 00000-0 24815-3 0 9993
2 12586 97.6838 137.1254 0019473 139.2073 221.0619 15.12045572224200
Epoch (UTC): | 22 May 2022 21:58:33 |
Eccentricity: | 0.0019473 |
inclination: | 97.6838° |
perigee height: | 516 km |
apogee height: | 543 km |
right ascension of ascending node: | 137.1254° |
argument of perigee: | 139.2073° |
revolutions per day: | 15.12045572 |
mean anomaly at epoch: | 221.0619° |
orbit number at epoch: | 22420 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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