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 44881U 19093C 22176.81720708 .00000583 00000-0 80512-4 0 9994
2 44881 97.8924 255.9058 0015568 154.1764 206.0219 14.81738684136014
Epoch (UTC): | 25 June 2022 19:36:46 |
Eccentricity: | 0.0015568 |
inclination: | 97.8924° |
perigee height: | 613 km |
apogee height: | 635 km |
right ascension of ascending node: | 255.9058° |
argument of perigee: | 154.1764° |
revolutions per day: | 14.81738684 |
mean anomaly at epoch: | 206.0219° |
orbit number at epoch: | 13601 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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