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 26906U 26075.60914558 +.00000000 +00000-0 +26486-3 0 00003
2 26906 63.4227 36.6233 0620193 341.5771 16.3657 13.45173364 06
| Epoch (UTC): | 16 March 2026 14:37:10 |
| Eccentricity: | 0.0620193 |
| inclination: | 63.4227° |
| perigee height: | 627 km |
| apogee height: | 1553 km |
| right ascension of ascending node: | 36.6233° |
| argument of perigee: | 341.5771° |
| revolutions per day: | 13.45173364 |
| mean anomaly at epoch: | 16.3657° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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