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 59911U 26145.62230687 +.00000000 +00000-0 +15127-3 0 00009
2 59911 44.9796 1.8477 0006523 144.8045 215.3219 13.99143799 03
| Epoch (UTC): | 25 May 2026 14:56:07 |
| Eccentricity: | 0.0006523 |
| inclination: | 44.9796° |
| perigee height: | 892 km |
| apogee height: | 902 km |
| right ascension of ascending node: | 1.8477° |
| argument of perigee: | 144.8045° |
| revolutions per day: | 13.99143799 |
| mean anomaly at epoch: | 215.3219° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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