View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 37736U 11031A 11202.20960648 -.00007606 00000-0 -74944-4 0 9996
2 37736 051.6428 349.4176 0010144 343.3446 020.7640 15.63375529 1966
| Epoch (UTC): | 21 July 2011 05:01:50 |
| Eccentricity: | 0.0010144 |
| inclination: | 51.6428° |
| perigee height: | 371 km |
| apogee height: | 385 km |
| right ascension of ascending node: | 349.4176° |
| argument of perigee: | 343.3446° |
| revolutions per day: | 15.63375529 |
| mean anomaly at epoch: | 20.7640° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|