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 43131U 18004W 22180.46571024 .00011907 00000-0 33357-3 0 9999
2 43131 97.3758 259.7751 0004429 306.2286 53.8548 15.36759759248425
Epoch (UTC): | 29 June 2022 11:10:37 |
Eccentricity: | 0.0004429 |
inclination: | 97.3758° |
perigee height: | 452 km |
apogee height: | 459 km |
right ascension of ascending node: | 259.7751° |
argument of perigee: | 306.2286° |
revolutions per day: | 15.36759759 |
mean anomaly at epoch: | 53.8548° |
orbit number at epoch: | 24842 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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