View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 32958U 08026A 14114.76726765 .00000170 00000-0 10104-3 0 9234
2 32958 098.5592 175.3910 0009981 015.8436 344.3051 14.19440114306263
| Epoch (UTC): | 24 April 2014 18:24:51 |
| Eccentricity: | 0.0009981 |
| inclination: | 98.5592° |
| perigee height: | 820 km |
| apogee height: | 834 km |
| right ascension of ascending node: | 175.3910° |
| argument of perigee: | 15.8436° |
| revolutions per day: | 14.19440114 |
| mean anomaly at epoch: | 344.3051° |
| orbit number at epoch: | 30626 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|