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 26136.24911104 +.00000000 +00000-0 +10569-1 0 00000
2 59588 97.1742 62.1881 0026580 350.8071 9.2605 13.92772823 04
| Epoch (UTC): | 16 May 2026 05:58:43 |
| Eccentricity: | 0.0026580 |
| inclination: | 97.1742° |
| perigee height: | 900 km |
| apogee height: | 938 km |
| right ascension of ascending node: | 62.1881° |
| argument of perigee: | 350.8071° |
| revolutions per day: | 13.92772823 |
| mean anomaly at epoch: | 9.2605° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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