View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43137U 18004AC 24033.82494968 .13075370 24468-5 25682-3 0 9994
2 43137 97.2729 126.2745 0011105 309.1902 50.8414 16.46500565338357
| Epoch (UTC): | 02 February 2024 19:47:55 |
| Eccentricity: | 0.0011105 |
| inclination: | 97.2729° |
| perigee height: | 141 km |
| apogee height: | 156 km |
| right ascension of ascending node: | 126.2745° |
| argument of perigee: | 309.1902° |
| revolutions per day: | 16.46500565 |
| mean anomaly at epoch: | 50.8414° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|