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 26016.46670005 +.00000000 +00000-0 +19063-3 0 00003
2 20580 28.4678 36.0194 0001775 244.4761 115.5651 15.28553314 04
| Epoch (UTC): | 16 January 2026 11:12:02 |
| Eccentricity: | 0.0001775 |
| inclination: | 28.4678° |
| perigee height: | 479 km |
| apogee height: | 481 km |
| right ascension of ascending node: | 36.0194° |
| argument of perigee: | 244.4761° |
| revolutions per day: | 15.28553314 |
| mean anomaly at epoch: | 115.5651° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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