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 59588U 26104.54937875 +.00000000 +00000-0 +21868-2 0 00006
2 59588 97.1910 37.6042 0072226 359.7596 0.3522 13.91258553 03
| Epoch (UTC): | 14 April 2026 13:11:06 |
| Eccentricity: | 0.0072226 |
| inclination: | 97.1910° |
| perigee height: | 871 km |
| apogee height: | 977 km |
| right ascension of ascending node: | 37.6042° |
| argument of perigee: | 359.7596° |
| revolutions per day: | 13.91258553 |
| mean anomaly at epoch: | 0.3522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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