View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 46320U 20061BA 22342.47112992 .00003182 00000-0 17909-3 0 9995
2 46320 97.4296 48.8173 0001279 268.1325 186.5146 15.13952691124843
| Epoch (UTC): | 08 December 2022 11:18:25 |
| Eccentricity: | 0.0001279 |
| inclination: | 97.4296° |
| perigee height: | 523 km |
| apogee height: | 525 km |
| right ascension of ascending node: | 48.8173° |
| argument of perigee: | 268.1325° |
| revolutions per day: | 15.13952691 |
| mean anomaly at epoch: | 186.5146° |
| orbit number at epoch: | 12484 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|