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 59856U 26145.59798558 +.00000000 +00000-0 -19315-4 0 00004
2 59856 43.0013 199.6109 0001584 276.8437 83.2234 15.27582524 09
| Epoch (UTC): | 25 May 2026 14:21:05 |
| Eccentricity: | 0.0001584 |
| inclination: | 43.0013° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 199.6109° |
| argument of perigee: | 276.8437° |
| revolutions per day: | 15.27582524 |
| mean anomaly at epoch: | 83.2234° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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