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 is defined by the following mean orbital elements,
1 21701U 91063B 11267.10904230 .15227068 11945-4 11522-3 0 9995
2 21701 056.9313 262.1789 0003645 318.1436 041.9334 16.52554649109189
| Epoch (UTC): | 24 September 2011 02:37:01 |
| Eccentricity: | 0.0003645 |
| inclination: | 56.9313° |
| perigee height: | 130 km |
| apogee height: | 135 km |
| right ascension of ascending node: | 262.1789° |
| argument of perigee: | 318.1436° |
| revolutions per day: | 16.52554649 |
| mean anomaly at epoch: | 41.9334° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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