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 40908U 15049K 24259.92250319 .00020715 00000-0 73354-3 0 9993
2 40908 97.5247 269.4429 0012748 41.1300 319.0898 15.29079634497345
| Epoch (UTC): | 15 September 2024 22:08:24 |
| Eccentricity: | 0.0012748 |
| inclination: | 97.5247° |
| perigee height: | 470 km |
| apogee height: | 487 km |
| right ascension of ascending node: | 269.4429° |
| argument of perigee: | 41.1300° |
| revolutions per day: | 15.29079634 |
| mean anomaly at epoch: | 319.0898° |
| orbit number at epoch: | 49734 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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