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 20580U 26101.49678816 +.00000000 +00000-0 +19678-3 0 00001
2 20580 28.4727 176.1109 0002351 124.7983 235.2834 15.30022712 07
| Epoch (UTC): | 11 April 2026 11:55:22 |
| Eccentricity: | 0.0002351 |
| inclination: | 28.4727° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 176.1109° |
| argument of perigee: | 124.7983° |
| revolutions per day: | 15.30022712 |
| mean anomaly at epoch: | 235.2834° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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