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 13142.85105921 .00004149 00000-0 38966-3 0 6146
2 00022 050.2858 294.0152 0161833 149.0711 003.3659 14.86590690839545
| Epoch (UTC): | 22 May 2013 20:25:31 |
| Eccentricity: | 0.0161833 |
| inclination: | 50.2858° |
| perigee height: | 495 km |
| apogee height: | 721 km |
| right ascension of ascending node: | 294.0152° |
| argument of perigee: | 149.0711° |
| revolutions per day: | 14.86590690 |
| mean anomaly at epoch: | 3.3659° |
| orbit number at epoch: | 83954 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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