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 21023.15859955 .00000492 00000-0 18885-4 0 9998
2 20580 28.4703 306.3836 0002474 298.4303 270.4737 15.09539991489288
| Epoch (UTC): | 23 January 2021 03:48:23 |
| Eccentricity: | 0.0002474 |
| inclination: | 28.4703° |
| perigee height: | 536 km |
| apogee height: | 539 km |
| right ascension of ascending node: | 306.3836° |
| argument of perigee: | 298.4303° |
| revolutions per day: | 15.09539991 |
| mean anomaly at epoch: | 270.4737° |
| orbit number at epoch: | 48928 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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