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 40889U 15045A 23330.39320127 -.00000016 00000-0 00000-0 0 9990
2 40889 55.3191 247.4036 0004874 11.8807 348.1585 1.70472934 51095
Epoch (UTC): | 26 November 2023 09:26:12 |
Eccentricity: | 0.0004874 |
inclination: | 55.3191° |
perigee height: | 23207 km |
apogee height: | 23236 km |
right ascension of ascending node: | 247.4036° |
argument of perigee: | 11.8807° |
revolutions per day: | 1.70472934 |
mean anomaly at epoch: | 348.1585° |
orbit number at epoch: | 5109 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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