View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 33506U 09004A 09114.86154729 .06921312 12321-4 12316-3 0 9990
2 33506 055.4370 280.8401 0011504 012.0650 349.7794 16.46787765 12981
| Epoch (UTC): | 24 April 2009 20:40:37 |
| Eccentricity: | 0.0011504 |
| inclination: | 55.4370° |
| perigee height: | 140 km |
| apogee height: | 155 km |
| right ascension of ascending node: | 280.8401° |
| argument of perigee: | 12.0650° |
| revolutions per day: | 16.46787765 |
| mean anomaly at epoch: | 349.7794° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|