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 59601U 26145.54678470 +.00000000 +00000-0 +23490-4 0 00005
2 59601 43.0010 324.1478 0000714 277.4635 82.6135 15.27575878 06
| Epoch (UTC): | 25 May 2026 13:07:22 |
| Eccentricity: | 0.0000714 |
| inclination: | 43.0010° |
| perigee height: | 483 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 324.1478° |
| argument of perigee: | 277.4635° |
| revolutions per day: | 15.27575878 |
| mean anomaly at epoch: | 82.6135° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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