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 59365U 26145.48068782 +.00000000 +00000-0 +32912-5 0 00004
2 59365 43.0009 186.4692 0001131 275.9149 84.1573 15.27581394 08
| Epoch (UTC): | 25 May 2026 11:32:11 |
| Eccentricity: | 0.0001131 |
| inclination: | 43.0009° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 186.4692° |
| argument of perigee: | 275.9149° |
| revolutions per day: | 15.27581394 |
| mean anomaly at epoch: | 84.1573° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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