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 26906U 01040B 24284.13804360 .00001151 00000-0 77218-3 0 9999
2 26906 63.4296 306.0146 0577177 340.2255 17.7188 13.44638673 20683
| Epoch (UTC): | 10 October 2024 03:18:46 |
| Eccentricity: | 0.0577177 |
| inclination: | 63.4296° |
| perigee height: | 661 km |
| apogee height: | 1523 km |
| right ascension of ascending node: | 306.0146° |
| argument of perigee: | 340.2255° |
| revolutions per day: | 13.44638673 |
| mean anomaly at epoch: | 17.7188° |
| orbit number at epoch: | 2068 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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