View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 28931U 06002A 13145.87274789 .00001001 00000-0 21605-3 0 1673
2 28931 098.0327 211.4998 0000809 046.7625 313.3627 14.60406988390783
| Epoch (UTC): | 25 May 2013 20:56:45 |
| Eccentricity: | 0.0000809 |
| inclination: | 98.0327° |
| perigee height: | 691 km |
| apogee height: | 692 km |
| right ascension of ascending node: | 211.4998° |
| argument of perigee: | 46.7625° |
| revolutions per day: | 14.60406988 |
| mean anomaly at epoch: | 313.3627° |
| orbit number at epoch: | 39078 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|