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 39026U 12072A 22221.89681261 .00016023 00000-0 42407-3 0 9994
2 39026 97.2696 212.0609 0027856 330.7106 29.2576 15.38058498537130
Epoch (UTC): | 09 August 2022 21:31:24 |
Eccentricity: | 0.0027856 |
inclination: | 97.2696° |
perigee height: | 433 km |
apogee height: | 471 km |
right ascension of ascending node: | 212.0609° |
argument of perigee: | 330.7106° |
revolutions per day: | 15.38058498 |
mean anomaly at epoch: | 29.2576° |
orbit number at epoch: | 53713 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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