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 59271U 26145.56802353 +.00000000 +00000-0 -13575-4 0 00003
2 59271 53.1598 170.7777 0000676 56.9623 303.1444 15.33559433 03
| Epoch (UTC): | 25 May 2026 13:37:57 |
| Eccentricity: | 0.0000676 |
| inclination: | 53.1598° |
| perigee height: | 465 km |
| apogee height: | 466 km |
| right ascension of ascending node: | 170.7777° |
| argument of perigee: | 56.9623° |
| revolutions per day: | 15.33559433 |
| mean anomaly at epoch: | 303.1444° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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