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 59931U 26145.37538566 +.00000000 +00000-0 +50278-4 0 00007
2 59931 43.0023 259.2053 0000925 241.8561 118.2197 15.27559533 04
| Epoch (UTC): | 25 May 2026 09:00:33 |
| Eccentricity: | 0.0000925 |
| inclination: | 43.0023° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 259.2053° |
| argument of perigee: | 241.8561° |
| revolutions per day: | 15.27559533 |
| mean anomaly at epoch: | 118.2197° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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