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 13145.90921936 .00001416 00000-0 17389-3 0 9160
2 26546 064.5575 286.7815 0045412 250.6253 254.0980 14.86514506685819
| Epoch (UTC): | 25 May 2013 21:49:16 |
| Eccentricity: | 0.0045412 |
| inclination: | 64.5575° |
| perigee height: | 577 km |
| apogee height: | 640 km |
| right ascension of ascending node: | 286.7815° |
| argument of perigee: | 250.6253° |
| revolutions per day: | 14.86514506 |
| mean anomaly at epoch: | 254.0980° |
| orbit number at epoch: | 68581 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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