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 00020U 59007A 13144.78736596 .00000460 00000-0 17395-3 0 2279
2 00020 033.3569 003.8030 1681829 274.8438 066.3005 11.52674179932207
| Epoch (UTC): | 24 May 2013 18:53:48 |
| Eccentricity: | 0.1681829 |
| inclination: | 33.3569° |
| perigee height: | 508 km |
| apogee height: | 3292 km |
| right ascension of ascending node: | 3.8030° |
| argument of perigee: | 274.8438° |
| revolutions per day: | 11.52674179 |
| mean anomaly at epoch: | 66.3005° |
| orbit number at epoch: | 93220 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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