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 26609U 00072B 13143.04078780 .00000023 00000-0 58046-1 0 8075
2 26609 006.7275 111.6291 7968892 352.9573 000.1373 01.25582801 57677
| Epoch (UTC): | 23 May 2013 00:58:44 |
| Eccentricity: | 0.7968892 |
| inclination: | 6.7275° |
| perigee height: | 992 km |
| apogee height: | 58829 km |
| right ascension of ascending node: | 111.6291° |
| argument of perigee: | 352.9573° |
| revolutions per day: | 1.25582801 |
| mean anomaly at epoch: | 0.1373° |
| orbit number at epoch: | 5767 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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