View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 65441U 26145.30941071 +.00000000 +00000-0 +28539-3 0 00006
2 65441 97.4559 359.4837 0002936 83.6903 276.4658 15.05660459 08
| Epoch (UTC): | 25 May 2026 07:25:33 |
| Eccentricity: | 0.0002936 |
| inclination: | 97.4559° |
| perigee height: | 547 km |
| apogee height: | 552 km |
| right ascension of ascending node: | 359.4837° |
| argument of perigee: | 83.6903° |
| revolutions per day: | 15.05660459 |
| mean anomaly at epoch: | 276.4658° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|