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 25198.68767456 -.00000034 00000-0 37036-4 0 9993
2 26906 63.4266 301.7758 0599917 340.8751 17.0585 13.44972298 58414
| Epoch (UTC): | 17 July 2025 16:30:15 |
| Eccentricity: | 0.0599917 |
| inclination: | 63.4266° |
| perigee height: | 643 km |
| apogee height: | 1539 km |
| right ascension of ascending node: | 301.7758° |
| argument of perigee: | 340.8751° |
| revolutions per day: | 13.44972298 |
| mean anomaly at epoch: | 17.0585° |
| orbit number at epoch: | 5841 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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