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 is defined by the following mean orbital elements,
1 26905U 01040A 26010.71573125 0.00000531 00000-0 26058-3 0 03
2 26905 63.3936 294.7006 0654650 11.0429 348.9047 13.41580911 03
| Epoch (UTC): | 10 January 2026 17:10:39 |
| Eccentricity: | 0.0654650 |
| inclination: | 63.3936° |
| perigee height: | 613 km |
| apogee height: | 1593 km |
| right ascension of ascending node: | 294.7006° |
| argument of perigee: | 11.0429° |
| revolutions per day: | 13.41580911 |
| mean anomaly at epoch: | 348.9047° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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