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 27422U 02021B 14203.74974172 .00000016 00000-0 22541-4 0 5422
2 27422 098.2977 244.5435 0013559 136.0001 000.7442 14.29034135635218
| Epoch (UTC): | 22 July 2014 17:59:37 |
| Eccentricity: | 0.0013559 |
| inclination: | 98.2977° |
| perigee height: | 785 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 244.5435° |
| argument of perigee: | 136.0001° |
| revolutions per day: | 14.29034135 |
| mean anomaly at epoch: | 0.7442° |
| orbit number at epoch: | 63521 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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