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 26549U 00057E 18344.71982299 -.00000016 00000-0 16093-4 0 9996
2 26549 64.5516 244.9641 0026394 346.6018 13.4384 14.83526625983978
| Epoch (UTC): | 10 December 2018 17:16:32 |
| Eccentricity: | 0.0026394 |
| inclination: | 64.5516° |
| perigee height: | 600 km |
| apogee height: | 636 km |
| right ascension of ascending node: | 244.9641° |
| argument of perigee: | 346.6018° |
| revolutions per day: | 14.83526625 |
| mean anomaly at epoch: | 13.4384° |
| orbit number at epoch: | 98397 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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