View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43546U 98067NU 20331.81655936 .13652478 12467-4 74947-3 0 9998
2 43546 51.6163 158.6708 0006544 274.8638 85.1642 16.42129147135921
| Epoch (UTC): | 26 November 2020 19:35:50 |
| Eccentricity: | 0.0006544 |
| inclination: | 51.6163° |
| perigee height: | 156 km |
| apogee height: | 164 km |
| right ascension of ascending node: | 158.6708° |
| argument of perigee: | 274.8638° |
| revolutions per day: | 16.42129147 |
| mean anomaly at epoch: | 85.1642° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|