View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 38096U 12010A 12276.81682870 .00016007 00000-0 26015-3 0 9999
2 38096 051.6482 306.4634 0007858 138.3310 215.8345 15.52835200 30144
| Epoch (UTC): | 02 October 2012 19:36:14 |
| Eccentricity: | 0.0007858 |
| inclination: | 51.6482° |
| perigee height: | 403 km |
| apogee height: | 414 km |
| right ascension of ascending node: | 306.4634° |
| argument of perigee: | 138.3310° |
| revolutions per day: | 15.52835200 |
| mean anomaly at epoch: | 215.8345° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|