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 65110U 26145.57387354 +.00000000 +00000-0 +11071-3 0 00009
2 65110 50.0050 46.7957 0009313 24.6326 335.4989 13.29321811 04
| Epoch (UTC): | 25 May 2026 13:46:22 |
| Eccentricity: | 0.0009313 |
| inclination: | 50.0050° |
| perigee height: | 1142 km |
| apogee height: | 1156 km |
| right ascension of ascending node: | 46.7957° |
| argument of perigee: | 24.6326° |
| revolutions per day: | 13.29321811 |
| mean anomaly at epoch: | 335.4989° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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