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 19017.10284584 .00000015 00000-0 23800-4 0 9992
2 27060 82.5406 135.0936 0007773 334.0785 25.9920 12.62997661786291
| Epoch (UTC): | 17 January 2019 02:28:05 |
| Eccentricity: | 0.0007773 |
| inclination: | 82.5406° |
| perigee height: | 1404 km |
| apogee height: | 1416 km |
| right ascension of ascending node: | 135.0936° |
| argument of perigee: | 334.0785° |
| revolutions per day: | 12.62997661 |
| mean anomaly at epoch: | 25.9920° |
| orbit number at epoch: | 78629 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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