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 22177.08732561 .00000548 00000-0 76105-4 0 9998
2 44881 97.8925 256.1721 0015587 153.3162 206.8830 14.81738669136053
Epoch (UTC): | 26 June 2022 02:05:44 |
Eccentricity: | 0.0015587 |
inclination: | 97.8925° |
perigee height: | 613 km |
apogee height: | 635 km |
right ascension of ascending node: | 256.1721° |
argument of perigee: | 153.3162° |
revolutions per day: | 14.81738669 |
mean anomaly at epoch: | 206.8830° |
orbit number at epoch: | 13605 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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