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 26130.78085779 +.00000000 +00000-0 +15182-3 0 00001
2 20580 28.4759 336.1432 0002200 84.0946 275.9901 15.30347678 06
| Epoch (UTC): | 10 May 2026 18:44:26 |
| Eccentricity: | 0.0002200 |
| inclination: | 28.4759° |
| perigee height: | 473 km |
| apogee height: | 476 km |
| right ascension of ascending node: | 336.1432° |
| argument of perigee: | 84.0946° |
| revolutions per day: | 15.30347678 |
| mean anomaly at epoch: | 275.9901° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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