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 13144.93368461 .00004656 00000-0 43387-3 0 6165
2 00022 050.2861 284.3722 0161745 156.9032 349.0857 14.86611485839859
| Epoch (UTC): | 24 May 2013 22:24:30 |
| Eccentricity: | 0.0161745 |
| inclination: | 50.2861° |
| perigee height: | 495 km |
| apogee height: | 721 km |
| right ascension of ascending node: | 284.3722° |
| argument of perigee: | 156.9032° |
| revolutions per day: | 14.86611485 |
| mean anomaly at epoch: | 349.0857° |
| orbit number at epoch: | 83985 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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