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 40912U 15049P 23265.79078675 .00080746 00000-0 12458-2 0 9999
2 40912 97.4098 286.1182 0009880 89.6923 270.5463 15.53815846444718
Epoch (UTC): | 22 September 2023 18:58:43 |
Eccentricity: | 0.0009880 |
inclination: | 97.4098° |
perigee height: | 399 km |
apogee height: | 412 km |
right ascension of ascending node: | 286.1182° |
argument of perigee: | 89.6923° |
revolutions per day: | 15.53815846 |
mean anomaly at epoch: | 270.5463° |
orbit number at epoch: | 44471 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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