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 27060U 01058F 18171.70454465 +.00000018 +00000-0 +41302-4 0 9995
2 27060 082.5400 270.1733 0009407 086.0290 274.1883 12.62996191759734
| Epoch (UTC): | 20 June 2018 16:54:32 |
| Eccentricity: | 0.0009407 |
| inclination: | 82.5400° |
| perigee height: | 1403 km |
| apogee height: | 1418 km |
| right ascension of ascending node: | 270.1733° |
| argument of perigee: | 86.0290° |
| revolutions per day: | 12.62996191 |
| mean anomaly at epoch: | 274.1883° |
| orbit number at epoch: | 75973 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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