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 61759U 26145.59283689 +.00000000 +00000-0 +17122-3 0 00005
2 61759 97.3258 346.5634 0007012 133.3554 226.8255 14.97789393 09
| Epoch (UTC): | 25 May 2026 14:13:41 |
| Eccentricity: | 0.0007012 |
| inclination: | 97.3258° |
| perigee height: | 569 km |
| apogee height: | 579 km |
| right ascension of ascending node: | 346.5634° |
| argument of perigee: | 133.3554° |
| revolutions per day: | 14.97789393 |
| mean anomaly at epoch: | 226.8255° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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