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 26071.73799039 +.00000000 +00000-0 +18958-1 0 00003
2 59588 97.2052 12.1643 0062273 69.1869 291.5951 13.89757757 09
| Epoch (UTC): | 12 March 2026 17:42:42 |
| Eccentricity: | 0.0062273 |
| inclination: | 97.2052° |
| perigee height: | 884 km |
| apogee height: | 975 km |
| right ascension of ascending node: | 12.1643° |
| argument of perigee: | 69.1869° |
| revolutions per day: | 13.89757757 |
| mean anomaly at epoch: | 291.5951° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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