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 59426U 26145.11307556 +.00000000 +00000-0 +18813-4 0 00000
2 59426 53.1590 77.3509 0000711 106.8783 253.2313 15.69709134 08
| Epoch (UTC): | 25 May 2026 02:42:49 |
| Eccentricity: | 0.0000711 |
| inclination: | 53.1590° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 77.3509° |
| argument of perigee: | 106.8783° |
| revolutions per day: | 15.69709134 |
| mean anomaly at epoch: | 253.2313° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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