View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 42729U 98067MJ 19037.76010169 .18316134 12568-4 56330-3 0 9997
2 42729 51.6029 213.2858 0007111 290.6627 69.5057 16.44582755 97544
| Epoch (UTC): | 06 February 2019 18:14:32 |
| Eccentricity: | 0.0007111 |
| inclination: | 51.6029° |
| perigee height: | 149 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 213.2858° |
| argument of perigee: | 290.6627° |
| revolutions per day: | 16.44582755 |
| mean anomaly at epoch: | 69.5057° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|