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 56541U 26145.48266637 +.00000000 +00000-0 +55786-4 0 00009
2 56541 43.0030 150.1552 0001149 274.6619 85.4102 15.27578849 08
| Epoch (UTC): | 25 May 2026 11:35:02 |
| Eccentricity: | 0.0001149 |
| inclination: | 43.0030° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 150.1552° |
| argument of perigee: | 274.6619° |
| revolutions per day: | 15.27578849 |
| mean anomaly at epoch: | 85.4102° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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