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 24278.48593413 .00001107 00000-0 74626-3 0 9995
2 26906 63.4308 320.5951 0576704 340.2167 17.7284 13.44626580 19925
| Epoch (UTC): | 04 October 2024 11:39:44 |
| Eccentricity: | 0.0576704 |
| inclination: | 63.4308° |
| perigee height: | 661 km |
| apogee height: | 1523 km |
| right ascension of ascending node: | 320.5951° |
| argument of perigee: | 340.2167° |
| revolutions per day: | 13.44626580 |
| mean anomaly at epoch: | 17.7284° |
| orbit number at epoch: | 1992 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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