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 59456U 26145.54085890 +.00000000 +00000-0 +23200-4 0 00000
2 59456 43.0035 320.7209 0001532 280.1894 79.8785 15.27575602 06
| Epoch (UTC): | 25 May 2026 12:58:50 |
| Eccentricity: | 0.0001532 |
| inclination: | 43.0035° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 320.7209° |
| argument of perigee: | 280.1894° |
| revolutions per day: | 15.27575602 |
| mean anomaly at epoch: | 79.8785° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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