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 26075.85896685 +.00000000 +00000-0 +21489-3 0 00000
2 20580 28.4725 351.0893 0001690 199.4729 160.5802 15.29601369 05
| Epoch (UTC): | 16 March 2026 20:36:54 |
| Eccentricity: | 0.0001690 |
| inclination: | 28.4725° |
| perigee height: | 476 km |
| apogee height: | 478 km |
| right ascension of ascending node: | 351.0893° |
| argument of perigee: | 199.4729° |
| revolutions per day: | 15.29601369 |
| mean anomaly at epoch: | 160.5802° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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