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 59222U 26145.42063845 +.00000000 +00000-0 +86342-5 0 00001
2 59222 53.1598 159.1898 0001054 86.4454 273.6667 15.30192450 02
| Epoch (UTC): | 25 May 2026 10:05:43 |
| Eccentricity: | 0.0001054 |
| inclination: | 53.1598° |
| perigee height: | 475 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 159.1898° |
| argument of perigee: | 86.4454° |
| revolutions per day: | 15.30192450 |
| mean anomaly at epoch: | 273.6667° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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