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 36574U 10020B 10192.71542822 .05314980 -55155-5 67545-3 0 9999
2 36574 029.9698 217.2715 0004364 151.2593 209.1628 16.34718051 8303
| Epoch (UTC): | 11 July 2010 17:10:12 |
| Eccentricity: | 0.0004364 |
| inclination: | 29.9698° |
| perigee height: | 177 km |
| apogee height: | 183 km |
| right ascension of ascending node: | 217.2715° |
| argument of perigee: | 151.2593° |
| revolutions per day: | 16.34718051 |
| mean anomaly at epoch: | 209.1628° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
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