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 56726U 26145.50507459 +.00000000 +00000-0 +82471-4 0 00008
2 56726 86.4506 66.2700 0002151 90.0750 270.0698 14.43311117 06
| Epoch (UTC): | 25 May 2026 12:07:18 |
| Eccentricity: | 0.0002151 |
| inclination: | 86.4506° |
| perigee height: | 746 km |
| apogee height: | 749 km |
| right ascension of ascending node: | 66.2700° |
| argument of perigee: | 90.0750° |
| revolutions per day: | 14.43311117 |
| mean anomaly at epoch: | 270.0698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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