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 59696U 26145.55178716 +.00000000 +00000-0 +92987-4 0 00005
2 59696 43.0012 346.1230 0001385 252.2066 107.8635 15.27579687 03
| Epoch (UTC): | 25 May 2026 13:14:34 |
| Eccentricity: | 0.0001385 |
| inclination: | 43.0012° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 346.1230° |
| argument of perigee: | 252.2066° |
| revolutions per day: | 15.27579687 |
| mean anomaly at epoch: | 107.8635° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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