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 19289.14400463 .00000412 00000-0 14147-4 0 9993
2 20580 28.4685 142.0338 0002600 333.4896 301.4473 15.09281468418958
| Epoch (UTC): | 16 October 2019 03:27:22 |
| Eccentricity: | 0.0002600 |
| inclination: | 28.4685° |
| perigee height: | 536 km |
| apogee height: | 540 km |
| right ascension of ascending node: | 142.0338° |
| argument of perigee: | 333.4896° |
| revolutions per day: | 15.09281468 |
| mean anomaly at epoch: | 301.4473° |
| orbit number at epoch: | 41895 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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