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 22826U 93061D 22179.09930246 .00000050 00000-0 36960-4 0 9996
2 22826 98.8802 210.2403 0009184 14.6277 345.5169 14.30523494500180
Epoch (UTC): | 28 June 2022 02:22:59 |
Eccentricity: | 0.0009184 |
inclination: | 98.8802° |
perigee height: | 783 km |
apogee height: | 796 km |
right ascension of ascending node: | 210.2403° |
argument of perigee: | 14.6277° |
revolutions per day: | 14.30523494 |
mean anomaly at epoch: | 345.5169° |
orbit number at epoch: | 50018 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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