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 1328U 65032A 18321.58940521 -.00000086 00000-0 -83943-5 0 9997
2 1328 41.1877 340.6588 0255263 304.6777 53.0164 13.38582494617724
| Epoch (UTC): | 17 November 2018 14:08:44 |
| Eccentricity: | 0.0255263 |
| inclination: | 41.1877° |
| perigee height: | 923 km |
| apogee height: | 1306 km |
| right ascension of ascending node: | 340.6588° |
| argument of perigee: | 304.6777° |
| revolutions per day: | 13.38582494 |
| mean anomaly at epoch: | 53.0164° |
| orbit number at epoch: | 61772 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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