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 61566U 26145.61515933 +.00000000 +00000-0 +23066-3 0 00008
2 61566 88.9830 60.5248 0007543 156.0855 204.0674 13.96689372 03
| Epoch (UTC): | 25 May 2026 14:45:49 |
| Eccentricity: | 0.0007543 |
| inclination: | 88.9830° |
| perigee height: | 900 km |
| apogee height: | 911 km |
| right ascension of ascending node: | 60.5248° |
| argument of perigee: | 156.0855° |
| revolutions per day: | 13.96689372 |
| mean anomaly at epoch: | 204.0674° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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