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 40911U 15049N 23079.24643723 .00020256 00000-0 80685-3 0 9991
2 40911 97.4942 87.0394 0014024 107.1603 309.2642 15.25172131414791
| Epoch (UTC): | 20 March 2023 05:54:52 |
| Eccentricity: | 0.0014024 |
| inclination: | 97.4942° |
| perigee height: | 480 km |
| apogee height: | 500 km |
| right ascension of ascending node: | 87.0394° |
| argument of perigee: | 107.1603° |
| revolutions per day: | 15.25172131 |
| mean anomaly at epoch: | 309.2642° |
| orbit number at epoch: | 41479 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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