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 22889U 93070B 23149.94295799 -.00000018 00000-0 -32262-4 0 9991
2 22889 82.9434 141.0216 0048356 258.3388 101.2340 13.78029034486601
Epoch (UTC): | 29 May 2023 22:37:51 |
Eccentricity: | 0.0048356 |
inclination: | 82.9434° |
perigee height: | 935 km |
apogee height: | 1006 km |
right ascension of ascending node: | 141.0216° |
argument of perigee: | 258.3388° |
revolutions per day: | 13.78029034 |
mean anomaly at epoch: | 101.2340° |
orbit number at epoch: | 48660 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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