View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 41313U 98067HP 18071.01090851 .37535990 12794-4 22365-3 0 9992
2 41313 51.6166 39.7363 0003024 270.6416 89.8040 16.54059622121479
| Epoch (UTC): | 12 March 2018 00:15:42 |
| Eccentricity: | 0.0003024 |
| inclination: | 51.6166° |
| perigee height: | 127 km |
| apogee height: | 130 km |
| right ascension of ascending node: | 39.7363° |
| argument of perigee: | 270.6416° |
| revolutions per day: | 16.54059622 |
| mean anomaly at epoch: | 89.8040° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|