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 59603U 26145.54501304 +.00000000 +00000-0 +13436-3 0 00006
2 59603 43.0025 327.5901 0001163 240.3887 119.6849 15.27578289 01
| Epoch (UTC): | 25 May 2026 13:04:49 |
| Eccentricity: | 0.0001163 |
| inclination: | 43.0025° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 327.5901° |
| argument of perigee: | 240.3887° |
| revolutions per day: | 15.27578289 |
| mean anomaly at epoch: | 119.6849° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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