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 26110.69356656 +.00000000 +00000-0 +15086-3 0 00007
2 20580 28.4731 113.3167 0001850 219.7473 140.2988 15.30092184 06
| Epoch (UTC): | 20 April 2026 16:38:44 |
| Eccentricity: | 0.0001850 |
| inclination: | 28.4731° |
| perigee height: | 474 km |
| apogee height: | 477 km |
| right ascension of ascending node: | 113.3167° |
| argument of perigee: | 219.7473° |
| revolutions per day: | 15.30092184 |
| mean anomaly at epoch: | 140.2988° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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