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 59717U 26145.15280875 +.00000000 +00000-0 -12133-4 0 00001
2 59717 53.1574 309.1851 0000894 11.1512 348.9526 15.69703739 02
| Epoch (UTC): | 25 May 2026 03:40:02 |
| Eccentricity: | 0.0000894 |
| inclination: | 53.1574° |
| perigee height: | 359 km |
| apogee height: | 360 km |
| right ascension of ascending node: | 309.1851° |
| argument of perigee: | 11.1512° |
| revolutions per day: | 15.69703739 |
| mean anomaly at epoch: | 348.9526° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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