View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00050U 60009B 22147.26627544 -.00000100 00000-0 -15052-3 0 9991
2 00050 47.2323 81.3418 0114225 278.4589 80.3268 12.20121531756767
| Epoch (UTC): | 27 May 2022 06:23:26 |
| Eccentricity: | 0.0114225 |
| inclination: | 47.2323° |
| perigee height: | 1501 km |
| apogee height: | 1683 km |
| right ascension of ascending node: | 81.3418° |
| argument of perigee: | 278.4589° |
| revolutions per day: | 12.20121531 |
| mean anomaly at epoch: | 80.3268° |
| orbit number at epoch: | 75676 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|