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 68593U 26145.58335647 +.00000000 +00000-0 -27793-2 0 00004
2 68593 51.8880 288.9177 0013119 317.7227 54.5589 14.99779942 06
| Epoch (UTC): | 25 May 2026 14:00:01 |
| Eccentricity: | 0.0013119 |
| inclination: | 51.8880° |
| perigee height: | 558 km |
| apogee height: | 577 km |
| right ascension of ascending node: | 288.9177° |
| argument of perigee: | 317.7227° |
| revolutions per day: | 14.99779942 |
| mean anomaly at epoch: | 54.5589° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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