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 24279U 96046C 13167.53431013 -.00000054 00000-0 -24055-4 0 5062
2 24279 098.7676 275.0375 0300910 056.3694 007.9479 13.46935713827469
| Epoch (UTC): | 16 June 2013 12:49:24 |
| Eccentricity: | 0.0300910 |
| inclination: | 98.7676° |
| perigee height: | 859 km |
| apogee height: | 1308 km |
| right ascension of ascending node: | 275.0375° |
| argument of perigee: | 56.3694° |
| revolutions per day: | 13.46935713 |
| mean anomaly at epoch: | 7.9479° |
| orbit number at epoch: | 82746 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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