View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit data is extracted from the following two-line orbital elements,
1 26093U 00004L 24260.93070709 .00008604 00000-0 18360-2 0 9991
2 26093 100.2042 249.2450 0024751 297.4315 62.4360 14.59015197299145
| Epoch (UTC): | 16 September 2024 22:20:13 |
| Eccentricity: | 0.0024751 |
| inclination: | 100.2042° |
| perigee height: | 679 km |
| apogee height: | 714 km |
| right ascension of ascending node: | 249.2450° |
| argument of perigee: | 297.4315° |
| revolutions per day: | 14.59015197 |
| mean anomaly at epoch: | 62.4360° |
| orbit number at epoch: | 29914 |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|