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 59768U 26145.39163275 +.00000000 +00000-0 +21173-2 0 00008
2 59768 53.1574 28.0635 0006758 137.3179 222.8352 15.40513129 08
| Epoch (UTC): | 25 May 2026 09:23:57 |
| Eccentricity: | 0.0006758 |
| inclination: | 53.1574° |
| perigee height: | 440 km |
| apogee height: | 449 km |
| right ascension of ascending node: | 28.0635° |
| argument of perigee: | 137.3179° |
| revolutions per day: | 15.40513129 |
| mean anomaly at epoch: | 222.8352° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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