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 65106U 26145.60746140 +.00000000 +00000-0 +11447-3 0 00007
2 65106 50.0042 46.9484 0008530 35.2134 324.9301 13.29317781 04
| Epoch (UTC): | 25 May 2026 14:34:44 |
| Eccentricity: | 0.0008530 |
| inclination: | 50.0042° |
| perigee height: | 1143 km |
| apogee height: | 1156 km |
| right ascension of ascending node: | 46.9484° |
| argument of perigee: | 35.2134° |
| revolutions per day: | 13.29317781 |
| mean anomaly at epoch: | 324.9301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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