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 41558U 16033C 22148.75100010 .00014830 00000-0 42091-3 0 9992
2 41558 97.4058 252.0146 0011658 81.0586 72.7788 15.36241056334627
Epoch (UTC): | 28 May 2022 18:01:26 |
Eccentricity: | 0.0011658 |
inclination: | 97.4058° |
perigee height: | 449 km |
apogee height: | 465 km |
right ascension of ascending node: | 252.0146° |
argument of perigee: | 81.0586° |
revolutions per day: | 15.36241056 |
mean anomaly at epoch: | 72.7788° |
orbit number at epoch: | 33462 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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