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 29499U 06044A 13140.42705324 .00000148 00000-0 87797-4 0 450
2 29499 098.7159 200.4580 0002057 146.7366 213.3941 14.21494001341636
| Epoch (UTC): | 20 May 2013 10:14:57 |
| Eccentricity: | 0.0002057 |
| inclination: | 98.7159° |
| perigee height: | 819 km |
| apogee height: | 822 km |
| right ascension of ascending node: | 200.4580° |
| argument of perigee: | 146.7366° |
| revolutions per day: | 14.21494001 |
| mean anomaly at epoch: | 213.3941° |
| orbit number at epoch: | 34163 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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