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 26064.23508279 +.00000000 +00000-0 +46467-3 0 00000
2 26906 63.4209 66.0300 0619203 341.5372 16.4044 13.45158044 04
| Epoch (UTC): | 05 March 2026 05:38:31 |
| Eccentricity: | 0.0619203 |
| inclination: | 63.4209° |
| perigee height: | 628 km |
| apogee height: | 1553 km |
| right ascension of ascending node: | 66.0300° |
| argument of perigee: | 341.5372° |
| revolutions per day: | 13.45158044 |
| mean anomaly at epoch: | 16.4044° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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