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 13340.71098341 .00002228 00000-0 26241-3 0 857
2 26546 064.5583 040.7191 0031386 227.0616 284.3690 14.87049319714777
| Epoch (UTC): | 06 December 2013 17:03:48 |
| Eccentricity: | 0.0031386 |
| inclination: | 64.5583° |
| perigee height: | 585 km |
| apogee height: | 629 km |
| right ascension of ascending node: | 40.7191° |
| argument of perigee: | 227.0616° |
| revolutions per day: | 14.87049319 |
| mean anomaly at epoch: | 284.3690° |
| orbit number at epoch: | 71477 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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