View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 40387U 15006A 15057.03324245 .22559532 12002-4 29842-3 0 9995
2 40387 055.5143 053.9122 0016447 231.3833 129.1773 16.47919074 3780
| Epoch (UTC): | 26 February 2015 00:47:52 |
| Eccentricity: | 0.0016447 |
| inclination: | 55.5143° |
| perigee height: | 134 km |
| apogee height: | 155 km |
| right ascension of ascending node: | 53.9122° |
| argument of perigee: | 231.3833° |
| revolutions per day: | 16.47919074 |
| mean anomaly at epoch: | 129.1773° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|