View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 43922U 26145.32165431 +.00000000 +00000-0 +19564-5 0 00006
2 43922 86.3986 3.1573 0002237 89.0930 271.0522 14.34217730 05
| Epoch (UTC): | 25 May 2026 07:43:10 |
| Eccentricity: | 0.0002237 |
| inclination: | 86.3986° |
| perigee height: | 776 km |
| apogee height: | 779 km |
| right ascension of ascending node: | 3.1573° |
| argument of perigee: | 89.0930° |
| revolutions per day: | 14.34217730 |
| mean anomaly at epoch: | 271.0522° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|