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 27057U 01058C 19017.12697154 .00000010 00000-0 -36821-5 0 9995
2 27057 82.5445 147.7465 0001794 87.0928 273.0368 12.61550745785386
| Epoch (UTC): | 17 January 2019 03:02:50 |
| Eccentricity: | 0.0001794 |
| inclination: | 82.5445° |
| perigee height: | 1415 km |
| apogee height: | 1418 km |
| right ascension of ascending node: | 147.7465° |
| argument of perigee: | 87.0928° |
| revolutions per day: | 12.61550745 |
| mean anomaly at epoch: | 273.0368° |
| orbit number at epoch: | 78538 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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