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 59037U 26145.52766848 +.00000000 +00000-0 +20547-3 0 00002
2 59037 43.0027 313.5557 0001550 258.0980 101.9698 15.27586008 00
| Epoch (UTC): | 25 May 2026 12:39:50 |
| Eccentricity: | 0.0001550 |
| inclination: | 43.0027° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 313.5557° |
| argument of perigee: | 258.0980° |
| revolutions per day: | 15.27586008 |
| mean anomaly at epoch: | 101.9698° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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