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 22178.50422084 .00000048 00000-0 34013-4 0 9998
2 20442 98.7943 143.5192 0012502 135.2679 224.9515 14.33066585694549
Epoch (UTC): | 27 June 2022 12:06:04 |
Eccentricity: | 0.0012502 |
inclination: | 98.7943° |
perigee height: | 772 km |
apogee height: | 790 km |
right ascension of ascending node: | 143.5192° |
argument of perigee: | 135.2679° |
revolutions per day: | 14.33066585 |
mean anomaly at epoch: | 224.9515° |
orbit number at epoch: | 69454 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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