View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 52191U 22033AL 24146.50949412 .15429445 25297-5 22962-3 0 9997
2 52191 97.2978 240.3180 0016695 271.5522 88.3869 16.47492065120493
| Epoch (UTC): | 25 May 2024 12:13:40 |
| Eccentricity: | 0.0016695 |
| inclination: | 97.2978° |
| perigee height: | 135 km |
| apogee height: | 157 km |
| right ascension of ascending node: | 240.3180° |
| argument of perigee: | 271.5522° |
| revolutions per day: | 16.47492065 |
| mean anomaly at epoch: | 88.3869° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|