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 24357.82542591 .00015904 00000-0 50082-3 0 9994
2 40908 97.5190 8.7007 0012433 50.3567 309.8769 15.32934628512323
| Epoch (UTC): | 22 December 2024 19:48:36 |
| Eccentricity: | 0.0012433 |
| inclination: | 97.5190° |
| perigee height: | 458 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 8.7007° |
| argument of perigee: | 50.3567° |
| revolutions per day: | 15.32934628 |
| mean anomaly at epoch: | 309.8769° |
| orbit number at epoch: | 51232 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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