View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 26473U 00047A 14056.12432529 0.00000300 00000-0 55593-4 0 04
2 26473 68.0114 73.0137 0005000 177.1720 182.8280 14.65191444 03
| Epoch (UTC): | 25 February 2014 02:59:01 |
| Eccentricity: | 0.0005000 |
| inclination: | 68.0114° |
| perigee height: | 673 km |
| apogee height: | 680 km |
| right ascension of ascending node: | 73.0137° |
| argument of perigee: | 177.1720° |
| revolutions per day: | 14.65191444 |
| mean anomaly at epoch: | 182.8280° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|