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 39120U 13011A 19107.90257576 +.00000096 +00000-0 +00000-0 0 9995
2 39120 002.6667 330.8011 0001993 062.0777 158.3750 01.00272650022311
| Epoch (UTC): | 17 April 2019 21:39:42 |
| Eccentricity: | 0.0001993 |
| inclination: | 2.6667° |
| perigee height: | 35777 km |
| apogee height: | 35794 km |
| right ascension of ascending node: | 330.8011° |
| argument of perigee: | 62.0777° |
| revolutions per day: | 1.00272650 |
| mean anomaly at epoch: | 158.3750° |
| orbit number at epoch: | 2231 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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