View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43197U 18015F 24231.21178278 .06806264 26318-5 86345-3 0 9993
2 43197 97.5713 57.2176 0008489 266.1265 93.9061 16.35917533365738
| Epoch (UTC): | 18 August 2024 05:04:58 |
| Eccentricity: | 0.0008489 |
| inclination: | 97.5713° |
| perigee height: | 171 km |
| apogee height: | 182 km |
| right ascension of ascending node: | 57.2176° |
| argument of perigee: | 266.1265° |
| revolutions per day: | 16.35917533 |
| mean anomaly at epoch: | 93.9061° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|