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 59350U 26145.49467684 +.00000000 +00000-0 +30939-4 0 00009
2 59350 43.0020 185.7226 0001128 280.9213 79.1512 15.27581809 02
| Epoch (UTC): | 25 May 2026 11:52:20 |
| Eccentricity: | 0.0001128 |
| inclination: | 43.0020° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 185.7226° |
| argument of perigee: | 280.9213° |
| revolutions per day: | 15.27581809 |
| mean anomaly at epoch: | 79.1512° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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