View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 24954U 97052B 23160.57939678 .00000109 00000-0 89688-4 0 9996
2 24954 82.9227 91.3343 0039433 174.2907 358.9072 13.80115196294768
| Epoch (UTC): | 09 June 2023 13:54:19 |
| Eccentricity: | 0.0039433 |
| inclination: | 82.9227° |
| perigee height: | 934 km |
| apogee height: | 992 km |
| right ascension of ascending node: | 91.3343° |
| argument of perigee: | 174.2907° |
| revolutions per day: | 13.80115196 |
| mean anomaly at epoch: | 358.9072° |
| orbit number at epoch: | 29476 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|