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 58759U 26145.62679067 +.00000000 +00000-0 +53480-3 0 00001
2 58759 49.9824 277.7545 0005407 200.5786 159.4950 15.17527734 08
| Epoch (UTC): | 25 May 2026 15:02:34 |
| Eccentricity: | 0.0005407 |
| inclination: | 49.9824° |
| perigee height: | 510 km |
| apogee height: | 517 km |
| right ascension of ascending node: | 277.7545° |
| argument of perigee: | 200.5786° |
| revolutions per day: | 15.17527734 |
| mean anomaly at epoch: | 159.4950° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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