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 56905U 26145.00284309 +.00000000 +00000-0 +17606-5 0 00007
2 56905 43.0051 359.3370 0001835 255.2870 104.7779 15.27587912 08
| Epoch (UTC): | 25 May 2026 00:04:05 |
| Eccentricity: | 0.0001835 |
| inclination: | 43.0051° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 359.3370° |
| argument of perigee: | 255.2870° |
| revolutions per day: | 15.27587912 |
| mean anomaly at epoch: | 104.7779° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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