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 26109.12818656 +.00000000 +00000-0 +14900-3 0 00000
2 20580 28.4728 124.0054 0001975 201.9875 158.0636 15.30079379 01
| Epoch (UTC): | 19 April 2026 03:04:35 |
| Eccentricity: | 0.0001975 |
| inclination: | 28.4728° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 124.0054° |
| argument of perigee: | 201.9875° |
| revolutions per day: | 15.30079379 |
| mean anomaly at epoch: | 158.0636° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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