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 26073.51012837 +.00000000 +00000-0 +33490-3 0 00005
2 20580 28.4725 7.1142 0001767 174.4342 185.6273 15.29568851 08
| Epoch (UTC): | 14 March 2026 12:14:35 |
| Eccentricity: | 0.0001767 |
| inclination: | 28.4725° |
| perigee height: | 476 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 7.1142° |
| argument of perigee: | 174.4342° |
| revolutions per day: | 15.29568851 |
| mean anomaly at epoch: | 185.6273° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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