View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43032U 26145.62772936 +.00000000 +00000-0 +45448-4 0 00004
2 43032 67.1462 247.3920 0006323 227.7307 132.3243 13.97425890 05
| Epoch (UTC): | 25 May 2026 15:03:55 |
| Eccentricity: | 0.0006323 |
| inclination: | 67.1462° |
| perigee height: | 898 km |
| apogee height: | 907 km |
| right ascension of ascending node: | 247.3920° |
| argument of perigee: | 227.7307° |
| revolutions per day: | 13.97425890 |
| mean anomaly at epoch: | 132.3243° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|