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 20U 59007A 19257.48566749 +.00000162 +00000-0 +50650-4 0 9995
2 20 033.3537 088.7278 1667249 237.5453 105.3083 11.55682401198553
| Epoch (UTC): | 14 September 2019 11:39:21 |
| Eccentricity: | 0.1667249 |
| inclination: | 33.3537° |
| perigee height: | 508 km |
| apogee height: | 3263 km |
| right ascension of ascending node: | 88.7278° |
| argument of perigee: | 237.5453° |
| revolutions per day: | 11.55682401 |
| mean anomaly at epoch: | 105.3083° |
| orbit number at epoch: | 19855 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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