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 25469U 98051C 13170.43706142 .00000250 00000-0 82372-4 0 2815
2 25469 086.3979 271.6848 0002246 110.7009 295.3271 14.34215578773756
| Epoch (UTC): | 19 June 2013 10:29:22 |
| Eccentricity: | 0.0002246 |
| inclination: | 86.3979° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 271.6848° |
| argument of perigee: | 110.7009° |
| revolutions per day: | 14.34215578 |
| mean anomaly at epoch: | 295.3271° |
| orbit number at epoch: | 77375 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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