View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 34380U 09011A 09067.01744983 +.00000005 +00000-0 +00000-0 0 9992
2 34380 028.5514 043.9608 2287689 108.4676 277.6729 07.34265484000068
| Epoch (UTC): | 08 March 2009 00:25:07 |
| Eccentricity: | 0.2287689 |
| inclination: | 28.5514° |
| perigee height: | 2245 km |
| apogee height: | 7361 km |
| right ascension of ascending node: | 43.9608° |
| argument of perigee: | 108.4676° |
| revolutions per day: | 7.34265484 |
| mean anomaly at epoch: | 277.6729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|