View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00047U 60007C 22022.28926839 .00000111 00000-0 49168-4 0 9994
2 00047 66.6659 33.7567 0233655 237.1743 120.6671 14.42224433218860
| Epoch (UTC): | 22 January 2022 06:56:32 |
| Eccentricity: | 0.0233655 |
| inclination: | 66.6659° |
| perigee height: | 584 km |
| apogee height: | 918 km |
| right ascension of ascending node: | 33.7567° |
| argument of perigee: | 237.1743° |
| revolutions per day: | 14.42224433 |
| mean anomaly at epoch: | 120.6671° |
| orbit number at epoch: | 21886 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|