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 data is extracted from the following two-line orbital elements,
1 20580U 90037B 21021.17309028 .00000492 00000-0 18889-4 0 9993
2 20580 28.4707 319.5184 0002456 275.3098 282.2701 15.09538791488827
| Epoch (UTC): | 21 January 2021 04:09:15 |
| Eccentricity: | 0.0002456 |
| inclination: | 28.4707° |
| perigee height: | 536 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 319.5184° |
| argument of perigee: | 275.3098° |
| revolutions per day: | 15.09538791 |
| mean anomaly at epoch: | 282.2701° |
| orbit number at epoch: | 48882 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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