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 58306U 26145.50246201 +.00000000 +00000-0 +47214-3 0 00004
2 58306 97.3815 236.9241 0005145 198.0260 162.0814 15.57652823 01
| Epoch (UTC): | 25 May 2026 12:03:32 |
| Eccentricity: | 0.0005145 |
| inclination: | 97.3815° |
| perigee height: | 391 km |
| apogee height: | 398 km |
| right ascension of ascending node: | 236.9241° |
| argument of perigee: | 198.0260° |
| revolutions per day: | 15.57652823 |
| mean anomaly at epoch: | 162.0814° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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