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 27875U 03040A 18196.49236183 0.00000000 00000-0 00000-0 0 00
2 27875 4.5092 68.0597 0003695 356.9613 3.0366 1.00270000 00
| Epoch (UTC): | 15 July 2018 11:49:00 |
| Eccentricity: | 0.0003695 |
| inclination: | 4.5092° |
| perigee height: | 35771 km |
| apogee height: | 35802 km |
| right ascension of ascending node: | 68.0597° |
| argument of perigee: | 356.9613° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 3.0366° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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