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 13141.15060383 -.00000008 00000-0 49328-4 0 4335
2 20480 099.0242 173.6171 0540886 162.3852 234.1022 12.83383900 90848
| Epoch (UTC): | 21 May 2013 03:36:52 |
| Eccentricity: | 0.0540886 |
| inclination: | 99.0242° |
| perigee height: | 911 km |
| apogee height: | 1744 km |
| right ascension of ascending node: | 173.6171° |
| argument of perigee: | 162.3852° |
| revolutions per day: | 12.83383900 |
| mean anomaly at epoch: | 234.1022° |
| orbit number at epoch: | 9084 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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