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 26071.22647860 +.00000000 +00000-0 +28559-3 0 00001
2 20580 28.4723 22.6938 0001818 150.2149 209.8550 15.29528665 01
| Epoch (UTC): | 12 March 2026 05:26:07 |
| Eccentricity: | 0.0001818 |
| inclination: | 28.4723° |
| perigee height: | 476 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 22.6938° |
| argument of perigee: | 150.2149° |
| revolutions per day: | 15.29528665 |
| mean anomaly at epoch: | 209.8550° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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