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 27598U 02056B 18173.43142606 -.00000009 00000-0 13263-4 0 9999
2 27598 98.4833 122.9010 0008107 230.8391 129.2072 14.28658150809207
| Epoch (UTC): | 22 June 2018 10:21:15 |
| Eccentricity: | 0.0008107 |
| inclination: | 98.4833° |
| perigee height: | 790 km |
| apogee height: | 802 km |
| right ascension of ascending node: | 122.9010° |
| argument of perigee: | 230.8391° |
| revolutions per day: | 14.28658150 |
| mean anomaly at epoch: | 129.2072° |
| orbit number at epoch: | 80920 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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