View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 35694U 09038F 10230.44082147 .07179566 12689-4 99310-4 0 9990
2 35694 051.5930 222.0149 0004218 308.0851 053.0105 16.48877011 61107
| Epoch (UTC): | 18 August 2010 10:34:46 |
| Eccentricity: | 0.0004218 |
| inclination: | 51.5930° |
| perigee height: | 139 km |
| apogee height: | 145 km |
| right ascension of ascending node: | 222.0149° |
| argument of perigee: | 308.0851° |
| revolutions per day: | 16.48877011 |
| mean anomaly at epoch: | 53.0105° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|