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 14071.11782572 .00000243 00000-0 11222-3 0 4353
2 27422 098.3120 118.1643 0013152 166.3981 246.6087 14.28969788616279
| Epoch (UTC): | 12 March 2014 02:49:40 |
| Eccentricity: | 0.0013152 |
| inclination: | 98.3120° |
| perigee height: | 786 km |
| apogee height: | 804 km |
| right ascension of ascending node: | 118.1643° |
| argument of perigee: | 166.3981° |
| revolutions per day: | 14.28969788 |
| mean anomaly at epoch: | 246.6087° |
| orbit number at epoch: | 61627 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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