View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 39026U 12072A 23034.39808876 .00037806 00000-0 73228-3 0 9992
2 39026 97.2814 29.0787 0026112 51.0536 309.3035 15.47240436564484
| Epoch (UTC): | 03 February 2023 09:33:14 |
| Eccentricity: | 0.0026112 |
| inclination: | 97.2814° |
| perigee height: | 407 km |
| apogee height: | 442 km |
| right ascension of ascending node: | 29.0787° |
| argument of perigee: | 51.0536° |
| revolutions per day: | 15.47240436 |
| mean anomaly at epoch: | 309.3035° |
| orbit number at epoch: | 56448 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|