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 25682U 99020A 13139.74774149 .00000412 00000-0 10150-3 0 1509
2 25682 098.1936 209.6044 0001091 115.4049 244.7255 14.57116836749697
| Epoch (UTC): | 19 May 2013 17:56:44 |
| Eccentricity: | 0.0001091 |
| inclination: | 98.1936° |
| perigee height: | 702 km |
| apogee height: | 703 km |
| right ascension of ascending node: | 209.6044° |
| argument of perigee: | 115.4049° |
| revolutions per day: | 14.57116836 |
| mean anomaly at epoch: | 244.7255° |
| orbit number at epoch: | 74969 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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