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 58937U 26145.49166625 +.00000000 +00000-0 +45732-4 0 00007
2 58937 53.1605 313.1270 0000945 89.0243 271.0866 15.30197377 08
| Epoch (UTC): | 25 May 2026 11:47:59 |
| Eccentricity: | 0.0000945 |
| inclination: | 53.1605° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 313.1270° |
| argument of perigee: | 89.0243° |
| revolutions per day: | 15.30197377 |
| mean anomaly at epoch: | 271.0866° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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