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 13143.92526324 .00006110 00000-0 56127-3 0 6159
2 00022 050.2860 289.0412 0161779 153.1040 352.2452 14.86598525839701
| Epoch (UTC): | 23 May 2013 22:12:22 |
| Eccentricity: | 0.0161779 |
| inclination: | 50.2860° |
| perigee height: | 495 km |
| apogee height: | 721 km |
| right ascension of ascending node: | 289.0412° |
| argument of perigee: | 153.1040° |
| revolutions per day: | 14.86598525 |
| mean anomaly at epoch: | 352.2452° |
| orbit number at epoch: | 83970 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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