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 26158.29828936 +.00000000 +00000-0 +18954-3 0 00007
2 20580 28.4712 148.1547 0001938 44.7656 315.3096 15.30642118 02
| Epoch (UTC): | 07 June 2026 07:09:32 |
| Eccentricity: | 0.0001938 |
| inclination: | 28.4712° |
| perigee height: | 473 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 148.1547° |
| argument of perigee: | 44.7656° |
| revolutions per day: | 15.30642118 |
| mean anomaly at epoch: | 315.3096° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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