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 26138.08457181 +.00000000 +00000-0 +16211-3 0 00006
2 20580 28.4749 286.2564 0001786 152.3712 207.6979 15.30409410 04
| Epoch (UTC): | 18 May 2026 02:01:47 |
| Eccentricity: | 0.0001786 |
| inclination: | 28.4749° |
| perigee height: | 473 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 286.2564° |
| argument of perigee: | 152.3712° |
| revolutions per day: | 15.30409410 |
| mean anomaly at epoch: | 207.6979° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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