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 56017U 26145.51508622 +.00000000 +00000-0 +28717-4 0 00008
2 56017 43.0065 331.4696 0001855 268.6659 91.3980 15.27575397 03
| Epoch (UTC): | 25 May 2026 12:21:43 |
| Eccentricity: | 0.0001855 |
| inclination: | 43.0065° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 331.4696° |
| argument of perigee: | 268.6659° |
| revolutions per day: | 15.27575397 |
| mean anomaly at epoch: | 91.3980° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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