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 56452U 26145.47159097 +.00000000 +00000-0 +27741-4 0 00000
2 56452 69.9987 311.0050 0002576 270.1804 89.9060 14.98332512 04
| Epoch (UTC): | 25 May 2026 11:19:05 |
| Eccentricity: | 0.0002576 |
| inclination: | 69.9987° |
| perigee height: | 570 km |
| apogee height: | 574 km |
| right ascension of ascending node: | 311.0050° |
| argument of perigee: | 270.1804° |
| revolutions per day: | 14.98332512 |
| mean anomaly at epoch: | 89.9060° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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