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 00022U 59009A 13140.83275510 .00005462 00000-0 50494-3 0 6121
2 00022 050.2856 303.3607 0161846 141.4415 002.0785 14.86566881839241
| Epoch (UTC): | 20 May 2013 19:59:10 |
| Eccentricity: | 0.0161846 |
| inclination: | 50.2856° |
| perigee height: | 495 km |
| apogee height: | 722 km |
| right ascension of ascending node: | 303.3607° |
| argument of perigee: | 141.4415° |
| revolutions per day: | 14.86566881 |
| mean anomaly at epoch: | 2.0785° |
| orbit number at epoch: | 83924 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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