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 22221.89681261 .00016023 00000-0 42407-3 0 9994
2 39026 97.2696 212.0609 0027856 330.7106 29.2576 15.38058498537130
| Epoch (UTC): | 09 August 2022 21:31:24 |
| Eccentricity: | 0.0027856 |
| inclination: | 97.2696° |
| perigee height: | 433 km |
| apogee height: | 471 km |
| right ascension of ascending node: | 212.0609° |
| argument of perigee: | 330.7106° |
| revolutions per day: | 15.38058498 |
| mean anomaly at epoch: | 29.2576° |
| orbit number at epoch: | 53713 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|