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 59093U 26145.61792073 +.00000000 +00000-0 +23114-3 0 00006
2 59093 42.9989 236.5098 0001813 272.1982 87.8662 15.27590924 07
| Epoch (UTC): | 25 May 2026 14:49:48 |
| Eccentricity: | 0.0001813 |
| inclination: | 42.9989° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 236.5098° |
| argument of perigee: | 272.1982° |
| revolutions per day: | 15.27590924 |
| mean anomaly at epoch: | 87.8662° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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