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 25400U 98043G 13140.05755171 .00000005 00000-0 19530-4 0 3772
2 25400 098.2916 132.6163 0009278 350.5042 009.5962 14.25188586772943
| Epoch (UTC): | 20 May 2013 01:22:52 |
| Eccentricity: | 0.0009278 |
| inclination: | 98.2916° |
| perigee height: | 801 km |
| apogee height: | 814 km |
| right ascension of ascending node: | 132.6163° |
| argument of perigee: | 350.5042° |
| revolutions per day: | 14.25188586 |
| mean anomaly at epoch: | 9.5962° |
| orbit number at epoch: | 77294 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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