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 59359U 26145.47684174 +.00000000 +00000-0 +20380-4 0 00000
2 59359 42.9994 186.4468 0001152 272.5418 87.5301 15.27574183 02
| Epoch (UTC): | 25 May 2026 11:26:39 |
| Eccentricity: | 0.0001152 |
| inclination: | 42.9994° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.4468° |
| argument of perigee: | 272.5418° |
| revolutions per day: | 15.27574183 |
| mean anomaly at epoch: | 87.5301° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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