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 27168U 02001A 18294.95978655 0.00000000 00000-0 00000-0 0 08
2 27168 8.1004 34.6674 0002928 164.1544 195.9778 1.00270000 01
| Epoch (UTC): | 21 October 2018 23:02:05 |
| Eccentricity: | 0.0002928 |
| inclination: | 8.1004° |
| perigee height: | 35774 km |
| apogee height: | 35799 km |
| right ascension of ascending node: | 34.6674° |
| argument of perigee: | 164.1544° |
| revolutions per day: | 1.00270000 |
| mean anomaly at epoch: | 195.9778° |
| 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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