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 26069.98675882 +.00000000 +00000-0 +29254-3 0 00009
2 20580 28.4718 31.1498 0001853 138.4359 221.6377 15.29506520 06
| Epoch (UTC): | 10 March 2026 23:40:55 |
| Eccentricity: | 0.0001853 |
| inclination: | 28.4718° |
| perigee height: | 476 km |
| apogee height: | 479 km |
| right ascension of ascending node: | 31.1498° |
| argument of perigee: | 138.4359° |
| revolutions per day: | 15.29506520 |
| mean anomaly at epoch: | 221.6377° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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