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 25199.57988655 -.00000025 00000-0 42300-4 0 9998
2 26906 63.4265 299.4715 0599995 340.8764 17.0571 13.44972509 58532
| Epoch (UTC): | 18 July 2025 13:55:02 |
| Eccentricity: | 0.0599995 |
| inclination: | 63.4265° |
| perigee height: | 642 km |
| apogee height: | 1539 km |
| right ascension of ascending node: | 299.4715° |
| argument of perigee: | 340.8764° |
| revolutions per day: | 13.44972509 |
| mean anomaly at epoch: | 17.0571° |
| orbit number at epoch: | 5853 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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