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 18140.92142792 -.00000019 +00000-0 +10425-3 0 9996
2 1328 041.1853 033.3113 0251841 085.2609 277.6854 13.38566002593081
| Epoch (UTC): | 20 May 2018 22:06:51 |
| Eccentricity: | 0.0251841 |
| inclination: | 41.1853° |
| perigee height: | 926 km |
| apogee height: | 1303 km |
| right ascension of ascending node: | 33.3113° |
| argument of perigee: | 85.2609° |
| revolutions per day: | 13.38566002 |
| mean anomaly at epoch: | 277.6854° |
| orbit number at epoch: | 59308 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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