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 5485U 71080A 18174.89787528 +.00000014 +00000-0 -37319-4 0 9996
2 5485 032.0549 115.8556 0640390 205.8400 150.8831 12.74129534177266
| Epoch (UTC): | 23 June 2018 21:32:56 |
| Eccentricity: | 0.0640390 |
| inclination: | 32.0549° |
| perigee height: | 869 km |
| apogee height: | 1861 km |
| right ascension of ascending node: | 115.8556° |
| argument of perigee: | 205.8400° |
| revolutions per day: | 12.74129534 |
| mean anomaly at epoch: | 150.8831° |
| orbit number at epoch: | 17726 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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