View from above orbital plane
|
View from above satellite
|
Ground track
|
The orbit is defined by the following mean orbital elements,
1 64565U 26144.88327769 +.00000000 +00000-0 +16436-3 0 00009
2 64565 97.7654 259.0766 0003484 41.6170 318.5314 14.93443202 06
| Epoch (UTC): | 24 May 2026 21:11:55 |
| Eccentricity: | 0.0003484 |
| inclination: | 97.7654° |
| perigee height: | 585 km |
| apogee height: | 590 km |
| right ascension of ascending node: | 259.0766° |
| argument of perigee: | 41.6170° |
| revolutions per day: | 14.93443202 |
| mean anomaly at epoch: | 318.5314° |
The dashed part of the orbit path shows where the satellite is in the earth's shadow,
|
|