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 20442U 90005G 22138.42726165 .00000204 00000-0 91131-4 0 9990
2 20442 98.7918 102.8339 0010605 256.0257 103.9747 14.33054532688802
Epoch (UTC): | 18 May 2022 10:15:15 |
Eccentricity: | 0.0010605 |
inclination: | 98.7918° |
perigee height: | 774 km |
apogee height: | 789 km |
right ascension of ascending node: | 102.8339° |
argument of perigee: | 256.0257° |
revolutions per day: | 14.33054532 |
mean anomaly at epoch: | 103.9747° |
orbit number at epoch: | 68880 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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