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 59108U 26145.56009866 +.00000000 +00000-0 +95860-4 0 00006
2 59108 97.8447 276.6706 0009436 73.2081 287.0175 14.96773019 08
| Epoch (UTC): | 25 May 2026 13:26:32 |
| Eccentricity: | 0.0009436 |
| inclination: | 97.8447° |
| perigee height: | 570 km |
| apogee height: | 583 km |
| right ascension of ascending node: | 276.6706° |
| argument of perigee: | 73.2081° |
| revolutions per day: | 14.96773019 |
| mean anomaly at epoch: | 287.0175° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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