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 18267.73135127 +.00000023 +00000-0 +68977-4 0 9998
2 27060 082.5417 208.5115 0007167 224.5638 211.4970 12.62997022771859
| Epoch (UTC): | 24 September 2018 17:33:08 |
| Eccentricity: | 0.0007167 |
| inclination: | 82.5417° |
| perigee height: | 1405 km |
| apogee height: | 1416 km |
| right ascension of ascending node: | 208.5115° |
| argument of perigee: | 224.5638° |
| revolutions per day: | 12.62997022 |
| mean anomaly at epoch: | 211.4970° |
| orbit number at epoch: | 77185 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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