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 59523U 26145.58238697 +.00000000 +00000-0 +30244-5 0 00001
2 59523 42.9974 243.9213 0001569 239.9441 120.1255 15.27580797 05
| Epoch (UTC): | 25 May 2026 13:58:38 |
| Eccentricity: | 0.0001569 |
| inclination: | 42.9974° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 243.9213° |
| argument of perigee: | 239.9441° |
| revolutions per day: | 15.27580797 |
| mean anomaly at epoch: | 120.1255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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