View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 22626U 93024A 13141.13338973 .00000913 00000-0 10429-3 0 7779
2 22626 082.5232 002.2271 0020227 016.2133 343.9726 14.84839015 85072
| Epoch (UTC): | 21 May 2013 03:12:04 |
| Eccentricity: | 0.0020227 |
| inclination: | 82.5232° |
| perigee height: | 600 km |
| apogee height: | 628 km |
| right ascension of ascending node: | 2.2271° |
| argument of perigee: | 16.2133° |
| revolutions per day: | 14.84839015 |
| mean anomaly at epoch: | 343.9726° |
| orbit number at epoch: | 8507 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|