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 3598U 68110B 22144.35753434 .00000526 00000-0 12430-3 0 9994
2 3598 34.9927 238.3146 0048528 89.4476 271.1777 14.54683452828993
Epoch (UTC): | 24 May 2022 08:34:50 |
Eccentricity: | 0.0048528 |
inclination: | 34.9927° |
perigee height: | 676 km |
apogee height: | 745 km |
right ascension of ascending node: | 238.3146° |
argument of perigee: | 89.4476° |
revolutions per day: | 14.54683452 |
mean anomaly at epoch: | 271.1777° |
orbit number at epoch: | 82899 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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