View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65226U 26145.41940497 +.00000000 +00000-0 +62956-4 0 00002
2 65226 10.9998 82.1472 0003346 9.5664 350.4627 14.29391329 09
| Epoch (UTC): | 25 May 2026 10:03:56 |
| Eccentricity: | 0.0003346 |
| inclination: | 10.9998° |
| perigee height: | 791 km |
| apogee height: | 796 km |
| right ascension of ascending node: | 82.1472° |
| argument of perigee: | 9.5664° |
| revolutions per day: | 14.29391329 |
| mean anomaly at epoch: | 350.4627° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|