View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 00029U 60002B 22269.61469025 .00000304 00000-0 75518-4 0 9990
2 00029 48.3810 345.3524 0024159 190.4628 169.5784 14.74740462341191
| Epoch (UTC): | 26 September 2022 14:45:09 |
| Eccentricity: | 0.0024159 |
| inclination: | 48.3810° |
| perigee height: | 629 km |
| apogee height: | 663 km |
| right ascension of ascending node: | 345.3524° |
| argument of perigee: | 190.4628° |
| revolutions per day: | 14.74740462 |
| mean anomaly at epoch: | 169.5784° |
| orbit number at epoch: | 34119 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|