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 59497U 26145.41048468 +.00000000 +00000-0 +45114-3 0 00008
2 59497 43.0012 266.9361 0000931 259.2847 100.7900 15.27524796 04
| Epoch (UTC): | 25 May 2026 09:51:05 |
| Eccentricity: | 0.0000931 |
| inclination: | 43.0012° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 266.9361° |
| argument of perigee: | 259.2847° |
| revolutions per day: | 15.27524796 |
| mean anomaly at epoch: | 100.7900° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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