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 62559U 26145.06717478 +.00000000 +00000-0 +16298-2 0 00006
2 62559 43.0028 39.6008 0002830 237.5799 122.4795 15.71018535 03
| Epoch (UTC): | 25 May 2026 01:36:43 |
| Eccentricity: | 0.0002830 |
| inclination: | 43.0028° |
| perigee height: | 354 km |
| apogee height: | 358 km |
| right ascension of ascending node: | 39.6008° |
| argument of perigee: | 237.5799° |
| revolutions per day: | 15.71018535 |
| mean anomaly at epoch: | 122.4795° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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