View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40458U 98067GB 15136.30676273 .20783109 12527-4 14817-2 0 9995
2 40458 051.6075 233.7697 0010355 318.5347 043.1720 16.39926603 21161
| Epoch (UTC): | 16 May 2015 07:21:44 |
| Eccentricity: | 0.0010355 |
| inclination: | 51.6075° |
| perigee height: | 159 km |
| apogee height: | 173 km |
| right ascension of ascending node: | 233.7697° |
| argument of perigee: | 318.5347° |
| revolutions per day: | 16.39926603 |
| mean anomaly at epoch: | 43.1720° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|