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 39026U 12072A 19201.16652273 .00000845 00000-0 33132-4 0 9990
2 39026 97.2108 203.2948 0037769 352.2712 7.7941 15.27872264366402
| Epoch (UTC): | 20 July 2019 03:59:47 |
| Eccentricity: | 0.0037769 |
| inclination: | 97.2108° |
| perigee height: | 456 km |
| apogee height: | 508 km |
| right ascension of ascending node: | 203.2948° |
| argument of perigee: | 352.2712° |
| revolutions per day: | 15.27872264 |
| mean anomaly at epoch: | 7.7941° |
| orbit number at epoch: | 36640 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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