View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42770U 17036F 17245.93730135 +.99999999 +00000-0 +73960-1 0 9995
2 42770 097.4262 306.2162 0014869 278.7167 080.9844 16.07641391010932
| Epoch (UTC): | 02 September 2017 22:29:42 |
| Eccentricity: | 0.0014869 |
| inclination: | 97.4262° |
| perigee height: | 243 km |
| apogee height: | 263 km |
| right ascension of ascending node: | 306.2162° |
| argument of perigee: | 278.7167° |
| revolutions per day: | 16.07641391 |
| mean anomaly at epoch: | 80.9844° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|