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 59891U 26145.42817947 +.00000000 +00000-0 +59139-4 0 00006
2 59891 43.0013 51.9584 0001175 273.9376 86.1342 15.27576586 04
| Epoch (UTC): | 25 May 2026 10:16:34 |
| Eccentricity: | 0.0001175 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 51.9584° |
| argument of perigee: | 273.9376° |
| revolutions per day: | 15.27576586 |
| mean anomaly at epoch: | 86.1342° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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