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 05917U 72022A 13138.87980247 .00000155 00000-0 82762-4 0 7163
2 05917 081.2297 255.9814 0032211 129.9485 017.8906 14.08439203112104
| Epoch (UTC): | 18 May 2013 21:06:54 |
| Eccentricity: | 0.0032211 |
| inclination: | 81.2297° |
| perigee height: | 841 km |
| apogee height: | 888 km |
| right ascension of ascending node: | 255.9814° |
| argument of perigee: | 129.9485° |
| revolutions per day: | 14.08439203 |
| mean anomaly at epoch: | 17.8906° |
| orbit number at epoch: | 11210 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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