View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 29655U 06058C 10216.61700559 .10637092 69904-5 33715-3 0 9992
2 29655 040.0059 067.3006 0005079 297.8744 064.7087 16.44862838207776
| Epoch (UTC): | 04 August 2010 14:48:29 |
| Eccentricity: | 0.0005079 |
| inclination: | 40.0059° |
| perigee height: | 149 km |
| apogee height: | 156 km |
| right ascension of ascending node: | 67.3006° |
| argument of perigee: | 297.8744° |
| revolutions per day: | 16.44862838 |
| mean anomaly at epoch: | 64.7087° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|