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 19200.90345424 +.00000320 +00000-0 +84960-5 0 9994
2 20580 028.4705 005.5496 0002853 099.8011 023.9881 15.09245854405528
| Epoch (UTC): | 19 July 2019 21:40:58 |
| Eccentricity: | 0.0002853 |
| inclination: | 28.4705° |
| perigee height: | 536 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 5.5496° |
| argument of perigee: | 99.8011° |
| revolutions per day: | 15.09245854 |
| mean anomaly at epoch: | 23.9881° |
| orbit number at epoch: | 40552 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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