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 22179.51839062 .00000473 00000-0 66635-4 0 9996
2 44881 97.8926 258.5679 0015771 145.6621 214.5617 14.81740631136412
Epoch (UTC): | 28 June 2022 12:26:28 |
Eccentricity: | 0.0015771 |
inclination: | 97.8926° |
perigee height: | 613 km |
apogee height: | 635 km |
right ascension of ascending node: | 258.5679° |
argument of perigee: | 145.6621° |
revolutions per day: | 14.81740631 |
mean anomaly at epoch: | 214.5617° |
orbit number at epoch: | 13641 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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