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 43937U 19003F 22177.58235501 .00011190 00000-0 37428-3 0 9996
2 43937 97.1293 210.5781 0022476 119.6172 240.7313 15.30893570191373
Epoch (UTC): | 26 June 2022 13:58:35 |
Eccentricity: | 0.0022476 |
inclination: | 97.1293° |
perigee height: | 458 km |
apogee height: | 488 km |
right ascension of ascending node: | 210.5781° |
argument of perigee: | 119.6172° |
revolutions per day: | 15.30893570 |
mean anomaly at epoch: | 240.7313° |
orbit number at epoch: | 19137 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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