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 26546U 00057B 14203.97980822 .00000288 00000-0 47711-4 0 3086
2 26546 064.5564 049.5501 0007426 229.0911 130.9555 14.88053470748728
| Epoch (UTC): | 22 July 2014 23:30:55 |
| Eccentricity: | 0.0007426 |
| inclination: | 64.5564° |
| perigee height: | 599 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 49.5501° |
| argument of perigee: | 229.0911° |
| revolutions per day: | 14.88053470 |
| mean anomaly at epoch: | 130.9555° |
| orbit number at epoch: | 74872 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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