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 14208.81859447 .00000595 00000-0 80895-4 0 3140
2 26546 064.5569 034.4638 0007003 231.9116 128.1362 14.88059443749448
| Epoch (UTC): | 27 July 2014 19:38:46 |
| Eccentricity: | 0.0007003 |
| inclination: | 64.5569° |
| perigee height: | 599 km |
| apogee height: | 609 km |
| right ascension of ascending node: | 34.4638° |
| argument of perigee: | 231.9116° |
| revolutions per day: | 14.88059443 |
| mean anomaly at epoch: | 128.1362° |
| orbit number at epoch: | 74944 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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