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 59536U 26145.36375005 +.00000000 +00000-0 +13471-3 0 00007
2 59536 42.9997 270.2521 0001108 295.1433 64.9304 15.27594873 03
| Epoch (UTC): | 25 May 2026 08:43:48 |
| Eccentricity: | 0.0001108 |
| inclination: | 42.9997° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 270.2521° |
| argument of perigee: | 295.1433° |
| revolutions per day: | 15.27594873 |
| mean anomaly at epoch: | 64.9304° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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