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 07493U 74083B 22142.87593585 -.00000006 00000-0 -10892-4 0 9998
2 07493 81.1622 199.0577 0080862 69.9871 290.9981 14.07625341441793
Epoch (UTC): | 22 May 2022 21:01:20 |
Eccentricity: | 0.0080862 |
inclination: | 81.1622° |
perigee height: | 809 km |
apogee height: | 926 km |
right ascension of ascending node: | 199.0577° |
argument of perigee: | 69.9871° |
revolutions per day: | 14.07625341 |
mean anomaly at epoch: | 290.9981° |
orbit number at epoch: | 44179 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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