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 59450U 26145.40977929 +.00000000 +00000-0 +92890-4 0 00003
2 59450 45.6195 35.8723 0003909 262.5488 97.4949 14.99057219 08
| Epoch (UTC): | 25 May 2026 09:50:04 |
| Eccentricity: | 0.0003909 |
| inclination: | 45.6195° |
| perigee height: | 567 km |
| apogee height: | 573 km |
| right ascension of ascending node: | 35.8723° |
| argument of perigee: | 262.5488° |
| revolutions per day: | 14.99057219 |
| mean anomaly at epoch: | 97.4949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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