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 26152.23451407 +.00000000 +00000-0 +18460-3 0 00002
2 20580 28.4714 189.5900 0001582 341.3793 18.6745 15.30573156 08
| Epoch (UTC): | 01 June 2026 05:37:42 |
| Eccentricity: | 0.0001582 |
| inclination: | 28.4714° |
| perigee height: | 473 km |
| apogee height: | 475 km |
| right ascension of ascending node: | 189.5900° |
| argument of perigee: | 341.3793° |
| revolutions per day: | 15.30573156 |
| mean anomaly at epoch: | 18.6745° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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