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 00050U 60009B 13142.34636148 -.00000125 00000-0 -37813-3 0 8989
2 00050 047.2296 218.1726 0114468 187.8321 172.0680 12.20075665355290
| Epoch (UTC): | 22 May 2013 08:18:45 |
| Eccentricity: | 0.0114468 |
| inclination: | 47.2296° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 218.1726° |
| argument of perigee: | 187.8321° |
| revolutions per day: | 12.20075665 |
| mean anomaly at epoch: | 172.0680° |
| orbit number at epoch: | 35529 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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