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 56407U 26145.39356321 +.00000000 +00000-0 -68355-4 0 00007
2 56407 43.0029 114.0061 0001197 272.5921 87.4793 15.27576856 01
| Epoch (UTC): | 25 May 2026 09:26:43 |
| Eccentricity: | 0.0001197 |
| inclination: | 43.0029° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 114.0061° |
| argument of perigee: | 272.5921° |
| revolutions per day: | 15.27576856 |
| mean anomaly at epoch: | 87.4793° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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