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 26138.20238654 +.00000000 +00000-0 +62859-4 0 00000
2 26906 63.4203 234.7772 0625417 341.7865 16.1628 13.45202425 06
| Epoch (UTC): | 18 May 2026 04:51:26 |
| Eccentricity: | 0.0625417 |
| inclination: | 63.4203° |
| perigee height: | 623 km |
| apogee height: | 1557 km |
| right ascension of ascending node: | 234.7772° |
| argument of perigee: | 341.7865° |
| revolutions per day: | 13.45202425 |
| mean anomaly at epoch: | 16.1628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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