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 26132.36933322 +.00000000 +00000-0 +13853-2 0 00005
2 59588 97.1739 59.1773 0035900 344.6924 15.3152 13.92302296 08
| Epoch (UTC): | 12 May 2026 08:51:50 |
| Eccentricity: | 0.0035900 |
| inclination: | 97.1739° |
| perigee height: | 894 km |
| apogee height: | 947 km |
| right ascension of ascending node: | 59.1773° |
| argument of perigee: | 344.6924° |
| revolutions per day: | 13.92302296 |
| mean anomaly at epoch: | 15.3152° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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