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 22180.84790241 .00000036 00000-0 31594-4 0 9992
2 22826 98.8800 212.0256 0009091 9.7055 350.4300 14.30523766500184
Epoch (UTC): | 29 June 2022 20:20:58 |
Eccentricity: | 0.0009091 |
inclination: | 98.8800° |
perigee height: | 783 km |
apogee height: | 796 km |
right ascension of ascending node: | 212.0256° |
argument of perigee: | 9.7055° |
revolutions per day: | 14.30523766 |
mean anomaly at epoch: | 350.4300° |
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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