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 18986U 88023B 23150.92705019 .00000055 00000-0 38909-4 0 9990
2 18986 82.9558 226.2396 0040562 233.6780 126.0630 13.78734402769871
Epoch (UTC): | 30 May 2023 22:14:57 |
Eccentricity: | 0.0040562 |
inclination: | 82.9558° |
perigee height: | 938 km |
apogee height: | 998 km |
right ascension of ascending node: | 226.2396° |
argument of perigee: | 233.6780° |
revolutions per day: | 13.78734402 |
mean anomaly at epoch: | 126.0630° |
orbit number at epoch: | 76987 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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