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 22237U 92080B 13138.82212723 .00000374 00000-0 49036-4 0 258
2 22237 082.5143 063.4724 0020738 040.8964 011.4949 14.77574176103290
| Epoch (UTC): | 18 May 2013 19:43:51 |
| Eccentricity: | 0.0020738 |
| inclination: | 82.5143° |
| perigee height: | 622 km |
| apogee height: | 651 km |
| right ascension of ascending node: | 63.4724° |
| argument of perigee: | 40.8964° |
| revolutions per day: | 14.77574176 |
| mean anomaly at epoch: | 11.4949° |
| orbit number at epoch: | 10329 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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