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 14205.15394804 -.00000042 00000-0 -13558-4 0 7917
2 20480 099.0468 161.3422 0539373 270.0552 155.5374 12.83394542145878
| Epoch (UTC): | 24 July 2014 03:41:41 |
| Eccentricity: | 0.0539373 |
| inclination: | 99.0468° |
| perigee height: | 912 km |
| apogee height: | 1743 km |
| right ascension of ascending node: | 161.3422° |
| argument of perigee: | 270.0552° |
| revolutions per day: | 12.83394542 |
| mean anomaly at epoch: | 155.5374° |
| orbit number at epoch: | 14587 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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