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 20465U 90010A 23159.47403306 .00002894 00000-0 22680-3 0 9998
2 20465 82.4875 307.1544 0015765 132.9832 227.2717 15.00546975790982
Epoch (UTC): | 08 June 2023 11:22:36 |
Eccentricity: | 0.0015765 |
inclination: | 82.4875° |
perigee height: | 554 km |
apogee height: | 576 km |
right ascension of ascending node: | 307.1544° |
argument of perigee: | 132.9832° |
revolutions per day: | 15.00546975 |
mean anomaly at epoch: | 227.2717° |
orbit number at epoch: | 79098 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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