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 24262.82784601 .00113899 00000-0 11345-2 0 9993
2 40911 97.4604 286.4192 0001193 312.7853 47.3305 15.65320313499128
| Epoch (UTC): | 18 September 2024 19:52:05 |
| Eccentricity: | 0.0001193 |
| inclination: | 97.4604° |
| perigee height: | 371 km |
| apogee height: | 373 km |
| right ascension of ascending node: | 286.4192° |
| argument of perigee: | 312.7853° |
| revolutions per day: | 15.65320313 |
| mean anomaly at epoch: | 47.3305° |
| orbit number at epoch: | 49912 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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