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 20480U 90013C 15059.75131257 -.00000019 00000-0 22524-4 0 9998
2 20480 099.0747 340.0110 0540865 132.8748 266.9094 12.83402107174042
| Epoch (UTC): | 28 February 2015 18:01:53 |
| Eccentricity: | 0.0540865 |
| inclination: | 99.0747° |
| perigee height: | 911 km |
| apogee height: | 1744 km |
| right ascension of ascending node: | 340.0110° |
| argument of perigee: | 132.8748° |
| revolutions per day: | 12.83402107 |
| mean anomaly at epoch: | 266.9094° |
| orbit number at epoch: | 17404 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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