View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 67448U 26145.32715450 +.00000000 +00000-0 +62124-3 0 00005
2 67448 43.0001 132.3626 0001408 268.1741 91.8949 15.27597672 05
| Epoch (UTC): | 25 May 2026 07:51:06 |
| Eccentricity: | 0.0001408 |
| inclination: | 43.0001° |
| perigee height: | 482 km |
| apogee height: | 484 km |
| right ascension of ascending node: | 132.3626° |
| argument of perigee: | 268.1741° |
| revolutions per day: | 15.27597672 |
| mean anomaly at epoch: | 91.8949° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|