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 27609U 02058E 18323.91404763 -.00000080 +00000-0 +92402-5 0 9991
2 27609 064.5557 203.3870 0055290 271.6620 087.8151 14.78479945858555
| Epoch (UTC): | 19 November 2018 21:56:13 |
| Eccentricity: | 0.0055290 |
| inclination: | 64.5557° |
| perigee height: | 595 km |
| apogee height: | 673 km |
| right ascension of ascending node: | 203.3870° |
| argument of perigee: | 271.6620° |
| revolutions per day: | 14.78479945 |
| mean anomaly at epoch: | 87.8151° |
| orbit number at epoch: | 85855 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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