View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43156U 18008B 24198.66905212 .17296646 24655-5 28398-3 0 9992
2 43156 97.2151 256.8209 0016593 258.3712 101.5729 16.46899832359648
| Epoch (UTC): | 16 July 2024 16:03:26 |
| Eccentricity: | 0.0016593 |
| inclination: | 97.2151° |
| perigee height: | 136 km |
| apogee height: | 158 km |
| right ascension of ascending node: | 256.8209° |
| argument of perigee: | 258.3712° |
| revolutions per day: | 16.46899832 |
| mean anomaly at epoch: | 101.5729° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|