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 05917U 26162.59251172 +.00000000 +00000-0 +10016-3 0 00005
2 05917 81.2304 290.6415 0050002 349.6619 10.3518 14.09281231 03
| Epoch (UTC): | 11 June 2026 14:13:13 |
| Eccentricity: | 0.0050002 |
| inclination: | 81.2304° |
| perigee height: | 826 km |
| apogee height: | 898 km |
| right ascension of ascending node: | 290.6415° |
| argument of perigee: | 349.6619° |
| revolutions per day: | 14.09281231 |
| mean anomaly at epoch: | 10.3518° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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