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 19460U 88078A 13130.18860101 0.00000160 00000-0 58508-4 0 04
2 19460 84.9876 11.9242 0003168 325.1896 34.8102 14.33037768 05
| Epoch (UTC): | 10 May 2013 04:31:35 |
| Eccentricity: | 0.0003168 |
| inclination: | 84.9876° |
| perigee height: | 779 km |
| apogee height: | 784 km |
| right ascension of ascending node: | 11.9242° |
| argument of perigee: | 325.1896° |
| revolutions per day: | 14.33037768 |
| mean anomaly at epoch: | 34.8102° |
| orbit number at epoch: | 0 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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